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 62626U 26145.49349531 +.00000000 +00000-0 +12006-4 0 00004
2 62626 97.3971 224.2804 0006618 75.4001 284.7967 15.17969710 09
| Epoch (UTC): | 25 May 2026 11:50:37 |
| Eccentricity: | 0.0006618 |
| inclination: | 97.3971° |
| perigee height: | 507 km |
| apogee height: | 517 km |
| right ascension of ascending node: | 224.2804° |
| argument of perigee: | 75.4001° |
| revolutions per day: | 15.17969710 |
| mean anomaly at epoch: | 284.7967° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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