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 62637U 26145.11512017 +.00000000 +00000-0 +33855-3 0 00000
2 62637 97.4022 227.4897 0003302 43.4912 316.6588 15.29382975 08
| Epoch (UTC): | 25 May 2026 02:45:46 |
| Eccentricity: | 0.0003302 |
| inclination: | 97.4022° |
| perigee height: | 475 km |
| apogee height: | 480 km |
| right ascension of ascending node: | 227.4897° |
| argument of perigee: | 43.4912° |
| revolutions per day: | 15.29382975 |
| mean anomaly at epoch: | 316.6588° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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