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 45741U 26145.49445712 +.00000000 +00000-0 +68734-3 0 00009
2 45741 53.0484 204.7479 0005901 348.6544 11.4335 15.63526215 02
| Epoch (UTC): | 25 May 2026 11:52:01 |
| Eccentricity: | 0.0005901 |
| inclination: | 53.0484° |
| perigee height: | 373 km |
| apogee height: | 381 km |
| right ascension of ascending node: | 204.7479° |
| argument of perigee: | 348.6544° |
| revolutions per day: | 15.63526215 |
| mean anomaly at epoch: | 11.4335° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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