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 28097U 03054C 25317.16840857 0.00000100 00000-0 67068-4 0 00
2 28097 63.3846 21.9418 0575274 6.3281 353.6719 13.41234080 03
| Epoch (UTC): | 13 November 2025 04:02:30 |
| Eccentricity: | 0.0575274 |
| inclination: | 63.3846° |
| perigee height: | 674 km |
| apogee height: | 1535 km |
| right ascension of ascending node: | 21.9418° |
| argument of perigee: | 6.3281° |
| revolutions per day: | 13.41234080 |
| mean anomaly at epoch: | 353.6719° |
| 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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