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 24932U 26087.23391823 +.00000000 +00000-0 +00000-0 0 00007
2 24932 13.6337 15.5253 0008111 38.2124 142.0078 0.98308748 06
| Epoch (UTC): | 28 March 2026 05:36:50 |
| Eccentricity: | 0.0008111 |
| inclination: | 13.6337° |
| perigee height: | 36311 km |
| apogee height: | 36381 km |
| right ascension of ascending node: | 15.5253° |
| argument of perigee: | 38.2124° |
| revolutions per day: | 0.98308748 |
| mean anomaly at epoch: | 142.0078° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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