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 62632U 26145.55025068 +.00000000 +00000-0 +19534-3 0 00006
2 62632 97.4006 226.0186 0004188 53.4670 306.6953 15.24335282 05
| Epoch (UTC): | 25 May 2026 13:12:21 |
| Eccentricity: | 0.0004188 |
| inclination: | 97.4006° |
| perigee height: | 490 km |
| apogee height: | 496 km |
| right ascension of ascending node: | 226.0186° |
| argument of perigee: | 53.4670° |
| revolutions per day: | 15.24335282 |
| mean anomaly at epoch: | 306.6953° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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