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 63042U 26145.58335647 +.00000000 +00000-0 -13992-3 0 00005
2 63042 53.1603 260.6950 0001042 92.7211 254.6790 15.33546699 06
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001042 |
| inclination: | 53.1603° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 260.6950° |
| argument of perigee: | 92.7211° |
| revolutions per day: | 15.33546699 |
| mean anomaly at epoch: | 254.6790° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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