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 68860U 26145.29293560 +.00000000 +00000-0 +39072-3 0 00009
2 68860 97.2854 159.9662 0002173 93.5183 266.6317 15.49225327 06
| Epoch (UTC): | 25 May 2026 07:01:49 |
| Eccentricity: | 0.0002173 |
| inclination: | 97.2854° |
| perigee height: | 418 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 159.9662° |
| argument of perigee: | 93.5183° |
| revolutions per day: | 15.49225327 |
| mean anomaly at epoch: | 266.6317° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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