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 68991U 26145.14176410 +.00000000 +00000-0 +14778-3 0 00008
2 68991 97.7389 43.0081 0002335 197.1083 163.0058 14.91058976 09
| Epoch (UTC): | 25 May 2026 03:24:08 |
| Eccentricity: | 0.0002335 |
| inclination: | 97.7389° |
| perigee height: | 593 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 43.0081° |
| argument of perigee: | 197.1083° |
| revolutions per day: | 14.91058976 |
| mean anomaly at epoch: | 163.0058° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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