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 68950U 26145.49283429 +.00000000 +00000-0 +63155-3 0 00003
2 68950 51.8768 176.9152 0003795 66.8440 293.2946 15.35939478 07
| Epoch (UTC): | 25 May 2026 11:49:40 |
| Eccentricity: | 0.0003795 |
| inclination: | 51.8768° |
| perigee height: | 456 km |
| apogee height: | 461 km |
| right ascension of ascending node: | 176.9152° |
| argument of perigee: | 66.8440° |
| revolutions per day: | 15.35939478 |
| mean anomaly at epoch: | 293.2946° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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