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 08293U 26088.19573350 +.00000000 +00000-0 +73938-4 0 00006
2 08293 81.2544 63.4691 0074421 194.2669 165.6404 14.12911306 06
| Epoch (UTC): | 29 March 2026 04:41:51 |
| Eccentricity: | 0.0074421 |
| inclination: | 81.2544° |
| perigee height: | 796 km |
| apogee height: | 903 km |
| right ascension of ascending node: | 63.4691° |
| argument of perigee: | 194.2669° |
| revolutions per day: | 14.12911306 |
| mean anomaly at epoch: | 165.6404° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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