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 62966U 26145.62627595 +.00000000 +00000-0 +81311-3 0 00009
2 62966 53.1610 235.3355 0001025 212.8833 147.2104 15.30214298 02
| Epoch (UTC): | 25 May 2026 15:01:50 |
| Eccentricity: | 0.0001025 |
| inclination: | 53.1610° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 235.3355° |
| argument of perigee: | 212.8833° |
| revolutions per day: | 15.30214298 |
| mean anomaly at epoch: | 147.2104° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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