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 62521U 26145.55530709 +.00000000 +00000-0 +14222-2 0 00004
2 62521 42.9859 327.7477 0001427 125.2852 234.8149 15.70910306 04
| Epoch (UTC): | 25 May 2026 13:19:38 |
| Eccentricity: | 0.0001427 |
| inclination: | 42.9859° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 327.7477° |
| argument of perigee: | 125.2852° |
| revolutions per day: | 15.70910306 |
| mean anomaly at epoch: | 234.8149° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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