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 26076.17076155 +.00000000 +00000-0 +24713-4 0 00003
2 08800 81.2541 348.2252 0094342 137.0351 223.8239 14.10651957 05
| Epoch (UTC): | 17 March 2026 04:05:53 |
| Eccentricity: | 0.0094342 |
| inclination: | 81.2541° |
| perigee height: | 789 km |
| apogee height: | 925 km |
| right ascension of ascending node: | 348.2252° |
| argument of perigee: | 137.0351° |
| revolutions per day: | 14.10651957 |
| mean anomaly at epoch: | 223.8239° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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