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 26160.29142074 +.00000000 +00000-0 +14587-4 0 00002
2 08800 81.2508 266.2975 0093390 258.9358 100.1299 14.10667974 00
| Epoch (UTC): | 09 June 2026 06:59:38 |
| Eccentricity: | 0.0093390 |
| inclination: | 81.2508° |
| perigee height: | 790 km |
| apogee height: | 925 km |
| right ascension of ascending node: | 266.2975° |
| argument of perigee: | 258.9358° |
| revolutions per day: | 14.10667974 |
| mean anomaly at epoch: | 100.1299° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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