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 45370U 26145.49071877 +.00000000 +00000-0 +94215-3 0 00007
2 45370 53.1559 167.9436 0004947 26.2147 333.9105 15.33594362 06
| Epoch (UTC): | 25 May 2026 11:46:38 |
| Eccentricity: | 0.0004947 |
| inclination: | 53.1559° |
| perigee height: | 462 km |
| apogee height: | 468 km |
| right ascension of ascending node: | 167.9436° |
| argument of perigee: | 26.2147° |
| revolutions per day: | 15.33594362 |
| mean anomaly at epoch: | 333.9105° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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