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 00876U 26071.71354373 +.00000000 +00000-0 +62912-4 0 00007
2 00876 65.0579 250.7982 0150197 296.9436 61.6389 14.65677254 00
| Epoch (UTC): | 12 March 2026 17:07:30 |
| Eccentricity: | 0.0150197 |
| inclination: | 65.0579° |
| perigee height: | 569 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 250.7982° |
| argument of perigee: | 296.9436° |
| revolutions per day: | 14.65677254 |
| mean anomaly at epoch: | 61.6389° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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