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 28095U 03054A 26002.77822294 0.00000252 00000-0 16463-3 0 02
2 28095 63.3928 238.1786 0577869 6.6046 353.3954 13.42020360 09
| Epoch (UTC): | 02 January 2026 18:40:38 |
| Eccentricity: | 0.0577869 |
| inclination: | 63.3928° |
| perigee height: | 669 km |
| apogee height: | 1534 km |
| right ascension of ascending node: | 238.1786° |
| argument of perigee: | 6.6046° |
| revolutions per day: | 13.42020360 |
| mean anomaly at epoch: | 353.3954° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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