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 45217U 26145.40688992 +.00000000 +00000-0 +12407-2 0 00002
2 45217 53.1590 27.0353 0002108 126.4597 233.6600 15.33735566 03
| Epoch (UTC): | 25 May 2026 09:45:55 |
| Eccentricity: | 0.0002108 |
| inclination: | 53.1590° |
| perigee height: | 463 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 27.0353° |
| argument of perigee: | 126.4597° |
| revolutions per day: | 15.33735566 |
| mean anomaly at epoch: | 233.6600° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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