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 56894U 26145.34548022 +.00000000 +00000-0 +14161-4 0 00008
2 56894 43.0054 15.7149 0000953 271.3823 88.6919 15.27580173 00
| Epoch (UTC): | 25 May 2026 08:17:29 |
| Eccentricity: | 0.0000953 |
| inclination: | 43.0054° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 15.7149° |
| argument of perigee: | 271.3823° |
| revolutions per day: | 15.27580173 |
| mean anomaly at epoch: | 88.6919° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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