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 45206U 26145.21128001 +.00000000 +00000-0 +10449-2 0 00003
2 45206 53.0404 321.8466 0008998 177.8159 182.2896 15.64119331 07
| Epoch (UTC): | 25 May 2026 05:04:14 |
| Eccentricity: | 0.0008998 |
| inclination: | 53.0404° |
| perigee height: | 370 km |
| apogee height: | 382 km |
| right ascension of ascending node: | 321.8466° |
| argument of perigee: | 177.8159° |
| revolutions per day: | 15.64119331 |
| mean anomaly at epoch: | 182.2896° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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