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 10515U 26088.19014122 +.00000000 +00000-0 +12705-3 0 00007
2 10515 81.2454 43.1651 0024496 196.4314 163.6065 14.09107309 02
| Epoch (UTC): | 29 March 2026 04:33:48 |
| Eccentricity: | 0.0024496 |
| inclination: | 81.2454° |
| perigee height: | 845 km |
| apogee height: | 880 km |
| right ascension of ascending node: | 43.1651° |
| argument of perigee: | 196.4314° |
| revolutions per day: | 14.09107309 |
| mean anomaly at epoch: | 163.6065° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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