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 26158.68799009 +.00000000 +00000-0 +10348-3 0 00001
2 00045 66.6942 25.3265 0246919 167.7935 192.9303 14.35959912 01
| Epoch (UTC): | 07 June 2026 16:30:42 |
| Eccentricity: | 0.0246919 |
| inclination: | 66.6942° |
| perigee height: | 595 km |
| apogee height: | 948 km |
| right ascension of ascending node: | 25.3265° |
| argument of perigee: | 167.7935° |
| revolutions per day: | 14.35959912 |
| mean anomaly at epoch: | 192.9303° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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