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 57362U 26145.46108904 +.00000000 +00000-0 -62482-4 0 00003
2 57362 43.0030 167.8428 0001637 279.3422 80.7245 15.27555575 00
| Epoch (UTC): | 25 May 2026 11:03:58 |
| Eccentricity: | 0.0001637 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 167.8428° |
| argument of perigee: | 279.3422° |
| revolutions per day: | 15.27555575 |
| mean anomaly at epoch: | 80.7245° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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