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 68639U 26144.77502061 +.00000000 +00000-0 -24205+1 0 00004
2 68639 88.9873 323.4151 0011474 75.2855 284.9574 13.64813415 00
| Epoch (UTC): | 24 May 2026 18:36:01 |
| Eccentricity: | 0.0011474 |
| inclination: | 88.9873° |
| perigee height: | 1010 km |
| apogee height: | 1027 km |
| right ascension of ascending node: | 323.4151° |
| argument of perigee: | 75.2855° |
| revolutions per day: | 13.64813415 |
| mean anomaly at epoch: | 284.9574° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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