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 02825U 67053B 25189.42482660 .00000033 00000-0 61363-4 0 9994
2 02825 69.9721 91.5088 0009616 262.9020 97.0993 13.97640033 44064
| Epoch (UTC): | 08 July 2025 10:11:45 |
| Eccentricity: | 0.0009616 |
| inclination: | 69.9721° |
| perigee height: | 895 km |
| apogee height: | 909 km |
| right ascension of ascending node: | 91.5088° |
| argument of perigee: | 262.9020° |
| revolutions per day: | 13.97640033 |
| mean anomaly at epoch: | 97.0993° |
| orbit number at epoch: | 4406 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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