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 25034U 97068A 25093.47239927 0.00000000 00000-0 00000-0 0 09
2 25034 64.6844 344.4956 6439229 271.7692 20.9108 2.00608404 06
| Epoch (UTC): | 03 April 2025 11:20:15 |
| Eccentricity: | 0.6439229 |
| inclination: | 64.6844° |
| perigee height: | 3078 km |
| apogee height: | 37278 km |
| right ascension of ascending node: | 344.4956° |
| argument of perigee: | 271.7692° |
| revolutions per day: | 2.00608404 |
| mean anomaly at epoch: | 20.9108° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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