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 08827U 26088.12222899 +.00000000 +00000-0 +15560-3 0 00007
2 08827 81.2675 44.3547 0014480 99.0870 261.1944 14.17023413 06
| Epoch (UTC): | 29 March 2026 02:56:00 |
| Eccentricity: | 0.0014480 |
| inclination: | 81.2675° |
| perigee height: | 825 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 44.3547° |
| argument of perigee: | 99.0870° |
| revolutions per day: | 14.17023413 |
| mean anomaly at epoch: | 261.1944° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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