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 46077U 26145.53412536 +.00000000 +00000-0 +12515-2 0 00000
2 46077 53.0232 74.1260 0002854 59.4836 300.6447 15.36808596 00
| Epoch (UTC): | 25 May 2026 12:49:08 |
| Eccentricity: | 0.0002854 |
| inclination: | 53.0232° |
| perigee height: | 454 km |
| apogee height: | 458 km |
| right ascension of ascending node: | 74.1260° |
| argument of perigee: | 59.4836° |
| revolutions per day: | 15.36808596 |
| mean anomaly at epoch: | 300.6447° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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