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 26161.84730213 +.00000000 +00000-0 +29290-4 0 00004
2 00876 65.0606 344.4443 0151906 265.4363 92.9374 14.65732308 06
| Epoch (UTC): | 10 June 2026 20:20:06 |
| Eccentricity: | 0.0151906 |
| inclination: | 65.0606° |
| perigee height: | 568 km |
| apogee height: | 782 km |
| right ascension of ascending node: | 344.4443° |
| argument of perigee: | 265.4363° |
| revolutions per day: | 14.65732308 |
| mean anomaly at epoch: | 92.9374° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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