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 53960U 26144.49390316 +.00000000 +00000-0 +00000-0 0 00008
2 53960 0.0468 94.6663 0001905 348.6628 233.4603 1.00269485 05
| Epoch (UTC): | 24 May 2026 11:51:13 |
| Eccentricity: | 0.0001905 |
| inclination: | 0.0468° |
| perigee height: | 35779 km |
| apogee height: | 35795 km |
| right ascension of ascending node: | 94.6663° |
| argument of perigee: | 348.6628° |
| revolutions per day: | 1.00269485 |
| mean anomaly at epoch: | 233.4603° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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