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 68972U 26145.58335647 +.00000000 +00000-0 -26838-1 0 00003
2 68972 53.1598 268.4713 0001522 86.6749 178.0045 15.50319426 07
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001522 |
| inclination: | 53.1598° |
| perigee height: | 415 km |
| apogee height: | 417 km |
| right ascension of ascending node: | 268.4713° |
| argument of perigee: | 86.6749° |
| revolutions per day: | 15.50319426 |
| mean anomaly at epoch: | 178.0045° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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