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 63853U 26144.99298086 +.00000000 +00000-0 +67401-3 0 00007
2 63853 43.0037 6.8003 0001467 274.6367 85.4317 15.27601071 02
| Epoch (UTC): | 24 May 2026 23:49:53 |
| Eccentricity: | 0.0001467 |
| inclination: | 43.0037° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 6.8003° |
| argument of perigee: | 274.6367° |
| revolutions per day: | 15.27601071 |
| mean anomaly at epoch: | 85.4317° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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