View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 51654U 26145.41449583 +.00000000 +00000-0 -71959-3 0 00005
2 51654 87.8859 40.7924 0001946 70.8736 289.2602 13.10370823 02
| Epoch (UTC): | 25 May 2026 09:56:52 |
| Eccentricity: | 0.0001946 |
| inclination: | 87.8859° |
| perigee height: | 1220 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.7924° |
| argument of perigee: | 70.8736° |
| revolutions per day: | 13.10370823 |
| mean anomaly at epoch: | 289.2602° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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