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 02802U 67045B 25342.91716622 .00000608 00000-0 17569-3 0 9999
2 02802 74.0096 157.6006 0064491 187.8239 172.1920 14.45530457 75908
| Epoch (UTC): | 08 December 2025 22:00:43 |
| Eccentricity: | 0.0064491 |
| inclination: | 74.0096° |
| perigee height: | 694 km |
| apogee height: | 786 km |
| right ascension of ascending node: | 157.6006° |
| argument of perigee: | 187.8239° |
| revolutions per day: | 14.45530457 |
| mean anomaly at epoch: | 172.1920° |
| orbit number at epoch: | 7590 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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