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 65470U 26144.61542470 +.00000000 +00000-0 +71561-3 0 00004
2 65470 53.1561 265.1313 0001937 91.4077 268.7147 15.31723481 04
| Epoch (UTC): | 24 May 2026 14:46:12 |
| Eccentricity: | 0.0001937 |
| inclination: | 53.1561° |
| perigee height: | 469 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 265.1313° |
| argument of perigee: | 91.4077° |
| revolutions per day: | 15.31723481 |
| mean anomaly at epoch: | 268.7147° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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