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 45189U 26145.44110897 +.00000000 +00000-0 +12289-2 0 00006
2 45189 53.1577 42.6213 0002859 118.9268 241.2021 15.33623901 09
| Epoch (UTC): | 25 May 2026 10:35:11 |
| Eccentricity: | 0.0002859 |
| inclination: | 53.1577° |
| perigee height: | 463 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 42.6213° |
| argument of perigee: | 118.9268° |
| revolutions per day: | 15.33623901 |
| mean anomaly at epoch: | 241.2021° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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