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 62896U 26145.33522610 +.00000000 +00000-0 +79107-3 0 00001
2 62896 42.9973 252.0112 0000362 330.2351 29.8480 15.27591397 08
| Epoch (UTC): | 25 May 2026 08:02:43 |
| Eccentricity: | 0.0000362 |
| inclination: | 42.9973° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 252.0112° |
| argument of perigee: | 330.2351° |
| revolutions per day: | 15.27591397 |
| mean anomaly at epoch: | 29.8480° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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