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 08800U 26072.90801003 +.00000000 +00000-0 +36489-4 0 00001
2 08800 81.2543 351.4012 0094116 146.2258 214.4959 14.10651538 04
| Epoch (UTC): | 13 March 2026 21:47:32 |
| Eccentricity: | 0.0094116 |
| inclination: | 81.2543° |
| perigee height: | 789 km |
| apogee height: | 925 km |
| right ascension of ascending node: | 351.4012° |
| argument of perigee: | 146.2258° |
| revolutions per day: | 14.10651538 |
| mean anomaly at epoch: | 214.4959° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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