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 45150U 26145.40123022 +.00000000 +00000-0 +11705-2 0 00006
2 45150 87.8858 40.8011 0001969 76.2276 283.9070 13.10371140 00
| Epoch (UTC): | 25 May 2026 09:37:46 |
| Eccentricity: | 0.0001969 |
| inclination: | 87.8858° |
| perigee height: | 1220 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.8011° |
| argument of perigee: | 76.2276° |
| revolutions per day: | 13.10371140 |
| mean anomaly at epoch: | 283.9070° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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