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 68986U 26145.46807832 +.00000000 +00000-0 +15320-3 0 00000
2 68986 97.7387 43.3484 0001768 142.8639 217.2702 14.91756547 01
| Epoch (UTC): | 25 May 2026 11:14:01 |
| Eccentricity: | 0.0001768 |
| inclination: | 97.7387° |
| perigee height: | 591 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 43.3484° |
| argument of perigee: | 142.8639° |
| revolutions per day: | 14.91756547 |
| mean anomaly at epoch: | 217.2702° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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