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 62720U 26141.06754666 +.00000000 +00000-0 +00000-0 0 00004
2 62720 29.7895 170.7713 4900292 266.7600 38.3968 3.84311335 06
| Epoch (UTC): | 21 May 2026 01:37:16 |
| Eccentricity: | 0.4900292 |
| inclination: | 29.7895° |
| perigee height: | 2402 km |
| apogee height: | 19275 km |
| right ascension of ascending node: | 170.7713° |
| argument of perigee: | 266.7600° |
| revolutions per day: | 3.84311335 |
| mean anomaly at epoch: | 38.3968° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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