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 45542U 26145.24155069 +.00000000 +00000-0 +10945-2 0 00004
2 45542 53.0444 80.1452 0006273 74.0499 286.1204 15.59383510 06
| Epoch (UTC): | 25 May 2026 05:47:49 |
| Eccentricity: | 0.0006273 |
| inclination: | 53.0444° |
| perigee height: | 385 km |
| apogee height: | 394 km |
| right ascension of ascending node: | 80.1452° |
| argument of perigee: | 74.0499° |
| revolutions per day: | 15.59383510 |
| mean anomaly at epoch: | 286.1204° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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