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 68750U 26145.58335647 +.00000000 +00000-0 +16058-2 0 00000
2 68750 97.2854 8.4381 0001454 85.6091 176.7598 15.33440698 06
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001454 |
| inclination: | 97.2854° |
| perigee height: | 465 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 8.4381° |
| argument of perigee: | 85.6091° |
| revolutions per day: | 15.33440698 |
| mean anomaly at epoch: | 176.7598° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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