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 45939U 26145.49347163 +.00000000 +00000-0 +20401-3 0 00008
2 45939 97.2843 213.9509 0005460 42.0401 318.1253 15.21319034 02
| Epoch (UTC): | 25 May 2026 11:50:35 |
| Eccentricity: | 0.0005460 |
| inclination: | 97.2843° |
| perigee height: | 498 km |
| apogee height: | 506 km |
| right ascension of ascending node: | 213.9509° |
| argument of perigee: | 42.0401° |
| revolutions per day: | 15.21319034 |
| mean anomaly at epoch: | 318.1253° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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