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 45212U 26145.06875464 +.00000000 +00000-0 +12802-2 0 00000
2 45212 53.0399 23.2614 0003721 60.7175 299.4194 15.26813428 00
| Epoch (UTC): | 25 May 2026 01:39:00 |
| Eccentricity: | 0.0003721 |
| inclination: | 53.0399° |
| perigee height: | 483 km |
| apogee height: | 488 km |
| right ascension of ascending node: | 23.2614° |
| argument of perigee: | 60.7175° |
| revolutions per day: | 15.26813428 |
| mean anomaly at epoch: | 299.4194° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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