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 68787U 26145.58335647 +.00000000 +00000-0 -27282-1 0 00001
2 68787 97.2851 182.4579 0001734 87.6609 93.0091 15.58741085 03
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001734 |
| inclination: | 97.2851° |
| perigee height: | 390 km |
| apogee height: | 392 km |
| right ascension of ascending node: | 182.4579° |
| argument of perigee: | 87.6609° |
| revolutions per day: | 15.58741085 |
| mean anomaly at epoch: | 93.0091° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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