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 43618U 26145.48337781 +.00000000 +00000-0 +23708-4 0 00008
2 43618 97.5068 18.0388 0001271 73.5080 286.6282 14.96189380 04
| Epoch (UTC): | 25 May 2026 11:36:03 |
| Eccentricity: | 0.0001271 |
| inclination: | 97.5068° |
| perigee height: | 578 km |
| apogee height: | 580 km |
| right ascension of ascending node: | 18.0388° |
| argument of perigee: | 73.5080° |
| revolutions per day: | 14.96189380 |
| mean anomaly at epoch: | 286.6282° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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