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 27868U 26145.56656894 +.00000000 +00000-0 +15043-3 0 00007
2 27868 82.4721 344.0389 0022366 104.1434 256.2134 12.45189759 08
| Epoch (UTC): | 25 May 2026 13:35:51 |
| Eccentricity: | 0.0022366 |
| inclination: | 82.4721° |
| perigee height: | 1467 km |
| apogee height: | 1502 km |
| right ascension of ascending node: | 344.0389° |
| argument of perigee: | 104.1434° |
| revolutions per day: | 12.45189759 |
| mean anomaly at epoch: | 256.2134° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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