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 68961U 26145.58335647 +.00000000 +00000-0 +43093-3 0 00004
2 68961 53.1591 268.7371 0001107 89.6511 45.1675 15.49297280 04
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001107 |
| inclination: | 53.1591° |
| perigee height: | 418 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 268.7371° |
| argument of perigee: | 89.6511° |
| revolutions per day: | 15.49297280 |
| mean anomaly at epoch: | 45.1675° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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