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 00899U 26053.65344727 +.00000000 +00000-0 +13744-3 0 00005
2 00899 79.6867 252.3306 0119649 140.6014 220.3916 13.83015967 04
| Epoch (UTC): | 22 February 2026 15:40:57 |
| Eccentricity: | 0.0119649 |
| inclination: | 79.6867° |
| perigee height: | 865 km |
| apogee height: | 1041 km |
| right ascension of ascending node: | 252.3306° |
| argument of perigee: | 140.6014° |
| revolutions per day: | 13.83015967 |
| mean anomaly at epoch: | 220.3916° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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