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 00812U 26110.86801477 +.00000000 +00000-0 +38790-4 0 00006
2 00812 99.8127 259.5046 0004812 243.7067 116.3614 14.24583808 09
| Epoch (UTC): | 20 April 2026 20:49:56 |
| Eccentricity: | 0.0004812 |
| inclination: | 99.8127° |
| perigee height: | 806 km |
| apogee height: | 813 km |
| right ascension of ascending node: | 259.5046° |
| argument of perigee: | 243.7067° |
| revolutions per day: | 14.24583808 |
| mean anomaly at epoch: | 116.3614° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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