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 45570U 26145.09927985 +.00000000 +00000-0 +11897-2 0 00009
2 45570 53.1562 81.0519 0005413 63.5423 296.6136 15.36784927 00
| Epoch (UTC): | 25 May 2026 02:22:57 |
| Eccentricity: | 0.0005413 |
| inclination: | 53.1562° |
| perigee height: | 452 km |
| apogee height: | 459 km |
| right ascension of ascending node: | 81.0519° |
| argument of perigee: | 63.5423° |
| revolutions per day: | 15.36784927 |
| mean anomaly at epoch: | 296.6136° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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