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 68982U 26145.27522177 +.00000000 +00000-0 +14102-3 0 00008
2 68982 97.7360 43.1358 0002634 214.2240 145.8809 14.91183832 06
| Epoch (UTC): | 25 May 2026 06:36:19 |
| Eccentricity: | 0.0002634 |
| inclination: | 97.7360° |
| perigee height: | 592 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 43.1358° |
| argument of perigee: | 214.2240° |
| revolutions per day: | 14.91183832 |
| mean anomaly at epoch: | 145.8809° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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