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 26725U 01012B 24337.36855641 -.00000083 00000-0 -20938-2 0 9990
2 26725 0.4536 205.0599 7056473 101.7704 306.4938 2.23578941193720
| Epoch (UTC): | 02 December 2024 08:50:43 |
| Eccentricity: | 0.7056473 |
| inclination: | 0.4536° |
| perigee height: | 894 km |
| apogee height: | 35759 km |
| right ascension of ascending node: | 205.0599° |
| argument of perigee: | 101.7704° |
| revolutions per day: | 2.23578941 |
| mean anomaly at epoch: | 306.4938° |
| orbit number at epoch: | 19372 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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