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 28537U 05004A 25197.96598627 0.00000000 00000-0 00000-0 0 03
2 28537 63.3900 205.7354 0517981 3.6842 356.3158 13.41167113 07
| Epoch (UTC): | 16 July 2025 23:11:01 |
| Eccentricity: | 0.0517981 |
| inclination: | 63.3900° |
| perigee height: | 717 km |
| apogee height: | 1492 km |
| right ascension of ascending node: | 205.7354° |
| argument of perigee: | 3.6842° |
| revolutions per day: | 13.41167113 |
| mean anomaly at epoch: | 356.3158° |
| 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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