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DECAYED

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GNOMES-2, 48910 (Decayed)

Orbit data source: Space-Track

GNOMES-2, 48910 was a payload satellite owned by PlanetiQ (US) in LEO that was launched on Wed, 30 Jun 2021 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

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<iframe src="https://www.satcat.com/sats-embedded/48910?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

Iframe URL

https://www.satcat.com/sats-embedded/48910?theme=dark&initialShowStats=false

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Identifier

48910, 2021-059AH

Orbit

Decayed

Last TLE update

11 months ago

Origin

Manufacturer

Blue Canyon

Mission

Decayed Commercial Communications

Bus & Motor

XSAT, Unknown motor

Mass

~30 kg wet, ~30 kg dry

Launch date (UTC)

2021-06-30 (4 years ago)

Launch vehicle

FALCON 9

Launch site

Air Force Eastern Test Range (AFETR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Box + 2 Pan, 0.6 m

Radar Cross Section

0.162 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 11 months ago

0 GNOMES-2
1 48910U 21059AH  24131.55719574  .17347472  27438-5  21614-3 0  9994
2 48910  97.5948 291.7408 0012035 255.9239 104.0727 16.49126212160263

Epoch: 2024-05-10T13:22Z

Definitive object data (Epoch: 2024-05-10T13:22:21.711Z)

Latitude

-0.00007°

Longitude

-137.68564°

Altitude

146.812 km

Speed

7.817 km/s

True Right ascension

19h 26m 57s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at TLE epoch

Visualization observer readout

No trajectory is available.

Visualization observer readout

No trajectory is available.

Orbital elements

Apogee altitude

146.285 km

Perigee altitude

130.599 km

Semi-major axis

6,516.579 km

Eccentricity

0.0012035

Inclination

97.5948°

RAAN

291.7408°

Arg. of periapsis

255.9239°

True anomaly

104.20642°

Mean anomaly

104.0727°

Eccentric anomaly

104.13957°

Mean motion

4.12585 °/min

BSTAR

0.00021614

Orbital period

87.25 mins

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Other satellites on launch #59 in the year 2021 (2021-06-30 UTC)

STARLINK-3003, 48879 (Decayed)

SPACEBEE-111, 48904 (Decayed)

NUSAT-19 (ROSALIND), 48905 (Decayed)

UMBRA-2001, 48906 (Decayed)

MANDRAKE 2 ABLE, 48907

MANDRAKE 2 BAKER, 48908

ION SCV-003, 48912 (Decayed)

CAPELLA-5 (WHITNEY), 48913 (Decayed)

ICEYE-X12, 48914 (Decayed)

ICEYE-X13, 48916

GNOMES-2 Visibility forecast

Observer location: undefined°, undefined°

Span	Click to sort rows by Start time (UTC) header in descending order	Start Az.	Max El. time (UTC)	Max El. Az.	Max El.	End time (UTC)	End Az.
4 mins	2025-04-22 18:33:10.234Z	204.644° SW	2025-04-22 18:35:10.234Z	281.301° WNW	40.432°	2025-04-22 18:37:10.234Z	346.691° N

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Check out GNOMES-2, 48910 (Decayed) on other resources

View GNOMES-2, 48910 (Decayed) on Celestrak

View GNOMES-2, 48910 (Decayed) on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

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