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 is defined by the following mean orbital elements,
1 29241U 06024B 24137.18458378 0.00000000 00000-0 00000-0 0 04
2 29241 10.2910 44.3916 0086030 266.9282 93.0718 0.98909832 08
| Epoch (UTC): | 16 May 2024 04:25:48 |
| Eccentricity: | 0.0086030 |
| inclination: | 10.2910° |
| perigee height: | 35806 km |
| apogee height: | 36538 km |
| right ascension of ascending node: | 44.3916° |
| argument of perigee: | 266.9282° |
| revolutions per day: | 0.98909832 |
| mean anomaly at epoch: | 93.0718° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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