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 25336U 98029A 23059.61226733 0.00000000 00000-0 00000-0 0 09
2 25336 7.7800 351.7371 0040495 303.4971 56.5029 1.00270000 06
| Epoch (UTC): | 28 February 2023 14:41:39 |
| Eccentricity: | 0.0040495 |
| inclination: | 7.7800° |
| perigee height: | 35616 km |
| apogee height: | 35957 km |
| right ascension of ascending node: | 351.7371° |
| argument of perigee: | 303.4971° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 56.5029° |
| 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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