TANSTAAFL-2, 62378
Orbit data source: Space-Track
TANSTAAFL-2, 62378 is a payload satellite owned by True Anomaly (US) in LEO that was launched on Sat, 21 Dec 2024 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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62378 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
True Anomaly
Mission
Operational Commercial Technology
Bus & Motor
JACKAL, Unknown motor
Mass
275 kg wet, 275 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 2.3 m
Radar Cross Section
1.240 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 TANSTAAFL-2
1 62378U 24247B 26282.56830970 .00008229 00000-0 27718-3 0 9992
2 62378 44.9871 25.2314 0002467 275.0801 84.9802 15.31244277100480Epoch: 2026-10-09T13:38Z
TLE epoch observation values (Epoch: 2026-10-09T13:38:21.958Z)
Latitude
0.00003°
Longitude
162.45201°
Altitude
471.949 km
Speed
7.632 km/s
True Right ascension
01h 40m 55s
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
02:53:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
475.403 km
Perigee altitude
472.022 km
Semi-major axis
6,851.85 km
Eccentricity
0.00025
Inclination
44.9871°
RAAN
25.2314°
Arg. of periapsis
275.0801°
True anomaly
85.00836°
Mean anomaly
84.9802°
Eccentric anomaly
84.99428°
Mean motion
3.82676 °/min
Orbital period
94.07 mins
BSTAR
0.00027718
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Other satellites on launch #247 in the year 2024 (2024-12-21 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.TANSTAAFL-2 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-10-10 10:11:45.957Z | 224.145° SW | 2026-10-10 10:14:45.957Z | 155.72° SSE | 51.297° | 2026-10-10 10:17:45.957Z | 76.229° E |
| 5 mins | 2026-10-10 11:51:45.957Z | 287.699° WNW | 2026-10-10 11:53:45.957Z | 3.893° NNE | 44.702° | 2026-10-10 11:56:45.957Z | 60.491° ENE |
| 5 mins | 2026-10-10 13:30:45.957Z | 314.1° NW | 2026-10-10 13:32:45.957Z | 18.641° NNE | 36.516° | 2026-10-10 13:35:45.957Z | 74.074° E |
| 6 mins | 2026-10-10 15:08:45.957Z | 295.135° NW | 2026-10-10 15:11:45.957Z | 103.336° ESE | 65.046° | 2026-10-10 15:14:45.957Z | 112.618° SE |
| 4 mins | 2026-10-10 16:47:45.957Z | 253.235° W | 2026-10-10 16:49:45.957Z | 212.46° SW | 19.13° | 2026-10-10 16:51:45.957Z | 176.688° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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