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 29249U 06027A 25061.43605570 0.00000030 00000-0 00000-0 0 01
2 29249 63.5688 295.0503 7092995 274.1647 14.7875 2.00618127 09
| Epoch (UTC): | 02 March 2025 10:27:55 |
| Eccentricity: | 0.7092995 |
| inclination: | 63.5688° |
| perigee height: | 1341 km |
| apogee height: | 39013 km |
| right ascension of ascending node: | 295.0503° |
| argument of perigee: | 274.1647° |
| revolutions per day: | 2.00618127 |
| mean anomaly at epoch: | 14.7875° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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