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 68976U 26145.58335647 +.00000000 +00000-0 -29503-1 0 00009
2 68976 53.1590 267.9440 0001378 63.7367 100.2229 15.60468269 07
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001378 |
| inclination: | 53.1590° |
| perigee height: | 385 km |
| apogee height: | 387 km |
| right ascension of ascending node: | 267.9440° |
| argument of perigee: | 63.7367° |
| revolutions per day: | 15.60468269 |
| mean anomaly at epoch: | 100.2229° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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