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 00045U 26083.81300396 +.00000000 +00000-0 +15324-3 0 00009
2 00045 66.6927 223.3665 0253620 222.0183 136.1221 14.35905091 03
| Epoch (UTC): | 24 March 2026 19:30:43 |
| Eccentricity: | 0.0253620 |
| inclination: | 66.6927° |
| perigee height: | 591 km |
| apogee height: | 953 km |
| right ascension of ascending node: | 223.3665° |
| argument of perigee: | 222.0183° |
| revolutions per day: | 14.35905091 |
| mean anomaly at epoch: | 136.1221° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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