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 data is extracted from the following two-line orbital elements,
1 28095U 03054A 25345.79636667 0.00000300 00000-0 19460-3 0 04
2 28095 63.3913 294.7879 0579973 6.6104 353.3896 13.42002254 04
| Epoch (UTC): | 11 December 2025 19:06:46 |
| Eccentricity: | 0.0579973 |
| inclination: | 63.3913° |
| perigee height: | 668 km |
| apogee height: | 1535 km |
| right ascension of ascending node: | 294.7879° |
| argument of perigee: | 6.6104° |
| revolutions per day: | 13.42002254 |
| mean anomaly at epoch: | 353.3896° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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