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 26105.88984676 +.00000000 +00000-0 +25152-4 0 00008
2 08800 81.2500 319.2885 0095126 53.4360 307.5519 14.10662471 06
| Epoch (UTC): | 15 April 2026 21:21:22 |
| Eccentricity: | 0.0095126 |
| inclination: | 81.2500° |
| perigee height: | 788 km |
| apogee height: | 926 km |
| right ascension of ascending node: | 319.2885° |
| argument of perigee: | 53.4360° |
| revolutions per day: | 14.10662471 |
| mean anomaly at epoch: | 307.5519° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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