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 26063.75809925 +.00000000 +00000-0 +37202-4 0 00009
2 08800 81.2538 0.3080 0093835 171.8534 188.4189 14.10649812 08
| Epoch (UTC): | 04 March 2026 18:11:39 |
| Eccentricity: | 0.0093835 |
| inclination: | 81.2538° |
| perigee height: | 789 km |
| apogee height: | 925 km |
| right ascension of ascending node: | 0.3080° |
| argument of perigee: | 171.8534° |
| revolutions per day: | 14.10649812 |
| mean anomaly at epoch: | 188.4189° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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