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 68781U 26145.58335647 +.00000000 +00000-0 -24450-1 0 00009
2 68781 97.2848 182.4561 0001740 90.0764 86.9977 15.61583043 07
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001740 |
| inclination: | 97.2848° |
| perigee height: | 382 km |
| apogee height: | 384 km |
| right ascension of ascending node: | 182.4561° |
| argument of perigee: | 90.0764° |
| revolutions per day: | 15.61583043 |
| mean anomaly at epoch: | 86.9977° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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