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 26016.45860072 +.00000000 +00000-0 +17096-3 0 00005
2 45370 53.0539 41.0952 0001440 77.8847 282.2303 15.06415110 01
| Epoch (UTC): | 16 January 2026 11:00:23 |
| Eccentricity: | 0.0001440 |
| inclination: | 53.0539° |
| perigee height: | 546 km |
| apogee height: | 548 km |
| right ascension of ascending node: | 41.0952° |
| argument of perigee: | 77.8847° |
| revolutions per day: | 15.06415110 |
| mean anomaly at epoch: | 282.2303° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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