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 65377U 26145.46747184 +.00000000 +00000-0 +79166-3 0 00002
2 65377 53.1595 171.3022 0001037 74.4317 285.6798 15.30198050 08
| Epoch (UTC): | 25 May 2026 11:13:09 |
| Eccentricity: | 0.0001037 |
| inclination: | 53.1595° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 171.3022° |
| argument of perigee: | 74.4317° |
| revolutions per day: | 15.30198050 |
| mean anomaly at epoch: | 285.6798° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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