IMECE, 56178
Orbit data source: Space-Track
IMECE, 56178 is a payload satellite owned by TUBITAK-UZAY (TR) in SSO that was launched on Sat, 15 Apr 2023 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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56178 intel report (Beta)
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Identifier
Orbit
Country
TR / TURKRelated business
Manufacturer
TUBITAK-UZAY
Mission
Operational Civil Imaging
Bus & Motor
IMECE, AOCS
Mass
800 kg wet, ~780 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Hex Cyl + 2 Pan, 4.0 m
Radar Cross Section
4.470 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 IMECE
1 56178U 23054A 26303.92131751 .00000164 00000-0 38813-4 0 9992
2 56178 98.1110 207.1330 0010933 100.3284 259.9153 14.65928407190290Epoch: 2026-10-30T22:06Z
TLE epoch observation values (Epoch: 2026-10-30T22:06:41.832Z)
Latitude
-0.00001°
Longitude
-163.77576°
Altitude
678.451 km
Speed
7.517 km/s
True Right ascension
13h 48m 31s
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
02:17:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
678.872 km
Perigee altitude
663.458 km
Semi-major axis
7,049.302 km
Eccentricity
0.00109
Inclination
98.111°
RAAN
207.133°
Arg. of periapsis
100.3284°
True anomaly
259.79198°
Mean anomaly
259.9153°
Eccentric anomaly
259.85364°
Mean motion
3.66711 °/min
Orbital period
98.17 mins
BSTAR
0.000038813
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Other satellites on launch #54 in the year 2023 (2023-04-15 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.IMECE 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-10-31 06:52:12.765Z | 3.104° NNE | 2026-10-31 06:56:12.765Z | 270.339° WNW | 58.836° | 2026-10-31 07:00:12.765Z | 207.737° SW |
| 7 mins | 2026-10-31 17:54:12.765Z | 180.447° SSW | 2026-10-31 17:57:12.765Z | 276.639° WNW | 65.93° | 2026-10-31 18:01:12.765Z | 340.931° N |
| 6 mins | 2026-11-01 05:50:12.765Z | 49.871° ENE | 2026-11-01 05:52:12.765Z | 85.226° E | 27.844° | 2026-11-01 05:56:12.765Z | 152.972° SSE |
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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