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 62677U 26145.20631115 +.00000000 +00000-0 +69817-3 0 00002
2 62677 97.3836 230.1594 0003887 59.5526 300.6104 15.40629128 00
| Epoch (UTC): | 25 May 2026 04:57:05 |
| Eccentricity: | 0.0003887 |
| inclination: | 97.3836° |
| perigee height: | 442 km |
| apogee height: | 447 km |
| right ascension of ascending node: | 230.1594° |
| argument of perigee: | 59.5526° |
| revolutions per day: | 15.40629128 |
| mean anomaly at epoch: | 300.6104° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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