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 28651U 05017C 25191.50411014 .00000632 00000-0 91284-4 0 9998
2 28651 97.8877 97.1124 0067308 333.6877 26.0920 14.78266424 84550
| Epoch (UTC): | 10 July 2025 12:05:55 |
| Eccentricity: | 0.0067308 |
| inclination: | 97.8877° |
| perigee height: | 587 km |
| apogee height: | 682 km |
| right ascension of ascending node: | 97.1124° |
| argument of perigee: | 333.6877° |
| revolutions per day: | 14.78266424 |
| mean anomaly at epoch: | 26.0920° |
| orbit number at epoch: | 8455 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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