BALKAN-2, 69024
Orbit data source: Space-Track
BALKAN-2, 69024 is a payload satellite owned by Endurosat (BG) in SSO that was launched on Sun, 03 May 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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69024 intel report (Beta)
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Identifier
Orbit
Country
BG / BGRRelated business
Manufacturer
Endurosat
Mission
Operational spacecraft
Bus & Motor
CUBESAT 16U, Unknown motor
Mass
32 kg wet, 32 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 14.5 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 BALKAN-2
1 69024U 26100AW 26174.94895534 .00004490 00000-0 21075-3 0 9992
2 69024 97.4064 72.6421 0003022 11.2908 348.8395 15.20143023 7832Epoch: 2026-06-23T22:46Z
TLE epoch observation values (Epoch: 2026-06-23T22:46:29.741Z)
Latitude
0.00004°
Longitude
178.90499°
Altitude
506.458 km
Speed
7.612 km/s
True Right ascension
04h 50m 34s
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
08:36:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.454 km
Perigee altitude
500.295 km
Semi-major axis
6,880.511 km
Eccentricity
0.0003
Inclination
97.4064°
RAAN
72.6421°
Arg. of periapsis
11.2908°
True anomaly
348.83279°
Mean anomaly
348.8395°
Eccentric anomaly
348.83615°
Mean motion
3.80288 °/min
Orbital period
94.67 mins
BSTAR
0.00021075
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Other satellites on launch #100 in the year 2026 (2026-05-03 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.BALKAN-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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-25 05:21:44.774Z | 42.305° NE | 2026-06-25 05:24:44.774Z | 100.946° ESE | 22.082° | 2026-06-25 05:26:44.774Z | 141.986° SSE |
| 4 mins | 2026-06-25 06:56:44.774Z | 322.457° NNW | 2026-06-25 06:58:44.774Z | 279.604° WNW | 18.545° | 2026-06-25 07:00:44.774Z | 245.367° WSW |
| 6 mins | 2026-06-25 17:32:44.774Z | 184.705° SSW | 2026-06-25 17:35:44.774Z | 235.658° WSW | 35.931° | 2026-06-25 17:38:44.774Z | 331.418° 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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