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 62133U 26145.48836242 +.00000000 +00000-0 +56782-3 0 00004
2 62133 43.0082 62.5200 0001620 268.0009 92.0657 15.27596371 08
| Epoch (UTC): | 25 May 2026 11:43:14 |
| Eccentricity: | 0.0001620 |
| inclination: | 43.0082° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 62.5200° |
| argument of perigee: | 268.0009° |
| revolutions per day: | 15.27596371 |
| mean anomaly at epoch: | 92.0657° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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