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 45072U 26144.74790447 +.00000000 +00000-0 +77268-3 0 00003
2 45072 53.1574 264.1217 0002569 322.7620 37.3204 15.33809755 07
| Epoch (UTC): | 24 May 2026 17:56:58 |
| Eccentricity: | 0.0002569 |
| inclination: | 53.1574° |
| perigee height: | 463 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 264.1217° |
| argument of perigee: | 322.7620° |
| revolutions per day: | 15.33809755 |
| mean anomaly at epoch: | 37.3204° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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