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 68108U 26145.63702164 +.00000000 +00000-0 +68159-3 0 00005
2 68108 97.2836 106.2299 0001037 96.2165 263.9196 15.33448281 04
| Epoch (UTC): | 25 May 2026 15:17:18 |
| Eccentricity: | 0.0001037 |
| inclination: | 97.2836° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 106.2299° |
| argument of perigee: | 96.2165° |
| revolutions per day: | 15.33448281 |
| mean anomaly at epoch: | 263.9196° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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