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 35815U 09047A 25093.83785948 0.00000000 00000-0 00000-0 0 06
2 35815 0.1323 155.1999 0013141 221.9118 138.0437 1.00263576 02
| Epoch (UTC): | 03 April 2025 20:06:31 |
| Eccentricity: | 0.0013141 |
| inclination: | 0.1323° |
| perigee height: | 35733 km |
| apogee height: | 35844 km |
| right ascension of ascending node: | 155.1999° |
| argument of perigee: | 221.9118° |
| revolutions per day: | 1.00263576 |
| mean anomaly at epoch: | 138.0437° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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