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 55370U 26145.64213900 +.00000000 +00000-0 +43999-4 0 00004
2 55370 43.0037 246.8116 0001467 280.8073 79.2614 15.27578214 04
| Epoch (UTC): | 25 May 2026 15:24:40 |
| Eccentricity: | 0.0001467 |
| inclination: | 43.0037° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 246.8116° |
| argument of perigee: | 280.8073° |
| revolutions per day: | 15.27578214 |
| mean anomaly at epoch: | 79.2614° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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