GGSE 2, 1244
Orbit data source: Space-Track
GGSE 2, 1244 is an American payload satellite in LEO that was launched on Tue, 09 Mar 1965 UTC via a THOR SLV-2 AGENA D launch vehicle from the Air Force Western Test Range (AFWTR). 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.
Request partner network tasking
Embed this page
1244 intel report (Beta)
Edit Public Description
Create New Watchlist
Expand to show TLE details & historyLast TLE update: 22 hours ago
TLE from 22 hours ago
0 GGSE 2
1 01244U 65016B 26127.80223524 .00000041 00000-0 67859-4 0 9997
2 01244 70.0789 272.3467 0019530 147.9332 212.2967 13.96154568112429TLE epoch observation values (Epoch: 2026-05-07T19:15:13.124Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #16 in the year 1965 (1965-03-09 UTC)
GGSE 2 Visibility forecast
Loading observer location...
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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-05-08 19:52:55.214Z | 353.01° N | 2026-05-08 19:57:55.214Z | 67.127° ENE | 32.73° | 2026-05-08 20:02:55.214Z | 127.217° SE |
| 8 mins | 2026-05-08 21:39:55.214Z | 300.692° NW | 2026-05-08 21:42:55.214Z | 257.087° W | 26.339° | 2026-05-08 21:47:55.214Z | 197.799° SSW |
| 10 mins | 2026-05-09 10:55:55.214Z | 205.427° SW | 2026-05-09 11:00:55.214Z | 3.172° NNE | 44.268° | 2026-05-09 11:05:55.214Z | 23.259° NE |
| 5 mins | 2026-05-09 12:44:55.214Z | 291.121° WNW | 2026-05-09 12:46:55.214Z | 313.148° NW | 14.703° | 2026-05-09 12:49:55.214Z | 344.924° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
|---|
Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
|---|