FEMTO-1, 68419
Orbit data source: Space-Track
FEMTO-1, 68419 is a Bulgarian payload satellite in SSO that was launched on Mon, 30 Mar 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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68419 intel report (Beta)
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Identifier
Orbit
Country
BG / BGRRelated business
Manufacturer
Endurosat
Mission
Operational Commercial Technology
Bus & Motor
CUBESAT 1U?, Unknown motor
Mass
~1 kg wet, ~1 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 14.5 m
Radar Cross Section
0.015 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 FEMTO-1
1 68419U 26067D 26217.44604148 .00002237 00000-0 10955-3 0 9995
2 68419 97.4573 175.3397 0003636 90.9167 269.2484 15.19197694 19423Epoch: 2026-08-05T10:42Z
TLE epoch observation values (Epoch: 2026-08-05T10:42:17.983Z)
Latitude
-0.00006°
Longitude
60.76445°
Altitude
511.386 km
Speed
7.608 km/s
True Right ascension
11h 41m 21s
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
22:10:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
507.736 km
Perigee altitude
502.73 km
Semi-major axis
6,883.37 km
Eccentricity
0.00036
Inclination
97.4573°
RAAN
175.3397°
Arg. of periapsis
90.9167°
True anomaly
269.20674°
Mean anomaly
269.2484°
Eccentric anomaly
269.22757°
Mean motion
3.80051 °/min
Orbital period
94.72 mins
BSTAR
0.00010955
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Other satellites on launch #67 in the year 2026 (2026-03-30 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.FEMTO-1 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-08-06 09:24:32.525Z | 43.644° NE | 2026-08-06 09:27:32.525Z | 103.138° ESE | 21.615° | 2026-08-06 09:29:32.525Z | 142.629° SSE |
| 4 mins | 2026-08-06 10:59:32.525Z | 322.307° NNW | 2026-08-06 11:00:32.525Z | 302.133° NW | 18.821° | 2026-08-06 11:03:32.525Z | 244.632° WSW |
| 5 mins | 2026-08-06 21:37:32.525Z | 197.093° SSW | 2026-08-06 21:39:32.525Z | 272.492° WNW | 36.918° | 2026-08-06 21:42:32.525Z | 335.052° NNW |
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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