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 62130U 26145.46652285 +.00000000 +00000-0 +64959-3 0 00007
2 62130 42.9991 62.3596 0000592 277.7573 82.3211 15.27595032 09
| Epoch (UTC): | 25 May 2026 11:11:47 |
| Eccentricity: | 0.0000592 |
| inclination: | 42.9991° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 62.3596° |
| argument of perigee: | 277.7573° |
| revolutions per day: | 15.27595032 |
| mean anomaly at epoch: | 82.3211° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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