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 68752U 26145.58335647 +.00000000 +00000-0 -33235-1 0 00008
2 68752 97.2848 9.2579 0001605 69.6783 327.3033 15.55654275 07
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001605 |
| inclination: | 97.2848° |
| perigee height: | 399 km |
| apogee height: | 401 km |
| right ascension of ascending node: | 9.2579° |
| argument of perigee: | 69.6783° |
| revolutions per day: | 15.55654275 |
| mean anomaly at epoch: | 327.3033° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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