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 68142U 26145.03245824 +.00000000 +00000-0 +33721-3 0 00009
2 68142 97.2858 166.6411 0000870 119.9898 240.1431 15.33447834 04
| Epoch (UTC): | 25 May 2026 00:46:44 |
| Eccentricity: | 0.0000870 |
| inclination: | 97.2858° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 166.6411° |
| argument of perigee: | 119.9898° |
| revolutions per day: | 15.33447834 |
| mean anomaly at epoch: | 240.1431° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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