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 08846U 26088.18084575 +.00000000 +00000-0 +73675-4 0 00003
2 08846 81.2230 70.3881 0036028 321.4639 38.3959 14.09012942 07
| Epoch (UTC): | 29 March 2026 04:20:25 |
| Eccentricity: | 0.0036028 |
| inclination: | 81.2230° |
| perigee height: | 837 km |
| apogee height: | 889 km |
| right ascension of ascending node: | 70.3881° |
| argument of perigee: | 321.4639° |
| revolutions per day: | 14.09012942 |
| mean anomaly at epoch: | 38.3959° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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