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 24944U 26088.08717169 +.00000000 +00000-0 +13572-3 0 00000
2 24944 86.3998 24.2686 0002367 85.6206 274.5262 14.36760103 00
| Epoch (UTC): | 29 March 2026 02:05:31 |
| Eccentricity: | 0.0002367 |
| inclination: | 86.3998° |
| perigee height: | 768 km |
| apogee height: | 771 km |
| right ascension of ascending node: | 24.2686° |
| argument of perigee: | 85.6206° |
| revolutions per day: | 14.36760103 |
| mean anomaly at epoch: | 274.5262° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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