SDA-NG-T1TL-320, 101002
Orbit data source: Space-Track
SDA-NG-T1TL-320, 101002 is an American payload satellite in LEO that was launched on Sat, 10 Oct 2026 UTC via an FALCON 9 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.
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101002 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
None
Manufacturer
Unknown
Mission
Operational spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 SDA-NG-T1TL-320
1 A1002U 26231V 26288.63150830 .00000152 00000-0 12078-3 0 9998
2 A1002 81.5012 195.8031 0009011 283.9414 76.0742 13.86302583 747Epoch: 2026-10-15T15:09Z
TLE epoch observation values (Epoch: 2026-10-15T15:09:22.317Z)
Latitude
-0°
Longitude
-55.70399°
Altitude
942.91 km
Speed
7.381 km/s
True Right ascension
13h 03m 12s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
17:45:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
945.404 km
Perigee altitude
932.218 km
Semi-major axis
7,316.948 km
Eccentricity
0.0009
Inclination
81.5012°
RAAN
195.8031°
Arg. of periapsis
283.9414°
True anomaly
76.17445°
Mean anomaly
76.0742°
Eccentric anomaly
76.12432°
Mean motion
3.46775 °/min
Orbital period
103.81 mins
BSTAR
0.00012078
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Other satellites on launch #231 in the year 2026 (2026-10-10 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.SDA-NG-T1TL-320 Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2026-10-16 05:35:22.688Z | 355.806° N | 2026-10-16 05:41:22.688Z | 106.332° ESE | 69.973° | 2026-10-16 05:46:22.688Z | 163.5° S |
| 5 mins | 2026-10-16 07:23:22.688Z | 295.951° NW | 2026-10-16 07:25:22.688Z | 273.94° WNW | 15.396° | 2026-10-16 07:28:22.688Z | 243.813° WSW |
| 6 mins | 2026-10-16 17:17:22.688Z | 111.391° ESE | 2026-10-16 17:20:22.688Z | 77.887° E | 16.736° | 2026-10-16 17:23:22.688Z | 47.6° ENE |
| 10 mins | 2026-10-16 18:59:22.688Z | 201.228° SSW | 2026-10-16 19:04:22.688Z | 300.56° NW | 64.884° | 2026-10-16 19:09:22.688Z | 1.987° NNE |
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 |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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