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 68910U 26145.29692392 +.00000000 +00000-0 +71687-3 0 00009
2 68910 97.2871 341.0715 0000886 67.4727 292.6617 15.49222335 05
| Epoch (UTC): | 25 May 2026 07:07:34 |
| Eccentricity: | 0.0000886 |
| inclination: | 97.2871° |
| perigee height: | 418 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 341.0715° |
| argument of perigee: | 67.4727° |
| revolutions per day: | 15.49222335 |
| mean anomaly at epoch: | 292.6617° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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