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 45074U 26145.34310825 +.00000000 +00000-0 +12174-2 0 00004
2 45074 53.1537 259.8591 0002708 280.6442 79.4257 15.37025648 03
| Epoch (UTC): | 25 May 2026 08:14:04 |
| Eccentricity: | 0.0002708 |
| inclination: | 53.1537° |
| perigee height: | 453 km |
| apogee height: | 457 km |
| right ascension of ascending node: | 259.8591° |
| argument of perigee: | 280.6442° |
| revolutions per day: | 15.37025648 |
| mean anomaly at epoch: | 79.4257° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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