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 68015U 26145.39459723 +.00000000 +00000-0 +49576-3 0 00007
2 68015 97.2845 94.3390 0001721 101.5276 258.6160 15.33447138 05
| Epoch (UTC): | 25 May 2026 09:28:13 |
| Eccentricity: | 0.0001721 |
| inclination: | 97.2845° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 94.3390° |
| argument of perigee: | 101.5276° |
| revolutions per day: | 15.33447138 |
| mean anomaly at epoch: | 258.6160° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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