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 65677U 26145.29888696 +.00000000 +00000-0 +33874-3 0 00006
2 65677 53.1603 349.7664 0001725 105.8303 254.2888 15.30201232 01
| Epoch (UTC): | 25 May 2026 07:10:23 |
| Eccentricity: | 0.0001725 |
| inclination: | 53.1603° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 349.7664° |
| argument of perigee: | 105.8303° |
| revolutions per day: | 15.30201232 |
| mean anomaly at epoch: | 254.2888° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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