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 35169U 99025DMZ 24355.01619700 .00003984 00000-0 78069-3 0 9999
2 35169 99.1694 197.2455 0159982 108.5045 253.3609 14.55559970605700
| Epoch (UTC): | 20 December 2024 00:23:19 |
| Eccentricity: | 0.0159982 |
| inclination: | 99.1694° |
| perigee height: | 594 km |
| apogee height: | 821 km |
| right ascension of ascending node: | 197.2455° |
| argument of perigee: | 108.5045° |
| revolutions per day: | 14.55559970 |
| mean anomaly at epoch: | 253.3609° |
| orbit number at epoch: | 60570 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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