EMISAR, 68427
Orbit data source: Space-Track
EMISAR, 68427 is a Romanian 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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68427 intel report (Beta)
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Identifier
Orbit
Country
RO / ROMRelated business
Manufacturer
RISERO
Mission
Operational spacecraft
Bus & Motor
CUBESAT 1U, Unknown motor
Mass
~1 kg wet, ~1 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 EMISAR
1 68427U 26067M 26171.39902397 .00006920 00000-0 33002-3 0 9995
2 68427 97.4550 129.9069 0001969 49.5250 310.6156 15.19404719 12438Epoch: 2026-06-20T09:34Z
TLE epoch observation values (Epoch: 2026-06-20T09:34:35.671Z)
Latitude
0°
Longitude
77.64406°
Altitude
509.844 km
Speed
7.609 km/s
True Right ascension
08h 39m 37s
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
15:15:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
505.962 km
Perigee altitude
503.252 km
Semi-major axis
6,882.744 km
Eccentricity
0.0002
Inclination
97.455°
RAAN
129.9069°
Arg. of periapsis
49.525°
True anomaly
310.59847°
Mean anomaly
310.6156°
Eccentric anomaly
310.60704°
Mean motion
3.80102 °/min
Orbital period
94.71 mins
BSTAR
0.00033002
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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.EMISAR 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 | 2026-06-22 09:33:44.480Z | 36.68° NE | 2026-06-22 09:36:44.480Z | 100.312° ESE | 27.098° | 2026-06-22 09:39:44.480Z | 159.23° S |
| 5 mins | 2026-06-22 21:46:44.480Z | 208.391° SW | 2026-06-22 21:48:44.480Z | 267.974° W | 30.782° | 2026-06-22 21:51:44.480Z | 328.827° NNW |
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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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 |
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