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 65503U 26144.87893564 +.00000000 +00000-0 +14313-4 0 00005
2 65503 53.1581 277.1995 0001039 95.1382 264.9737 15.30192211 08
| Epoch (UTC): | 24 May 2026 21:05:40 |
| Eccentricity: | 0.0001039 |
| inclination: | 53.1581° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 277.1995° |
| argument of perigee: | 95.1382° |
| revolutions per day: | 15.30192211 |
| mean anomaly at epoch: | 264.9737° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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