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 00053U 26107.90098549 +.00000000 +00000-0 +43224-3 0 00009
2 00053 47.2766 168.3008 0101015 257.1061 101.8429 12.17409357 02
| Epoch (UTC): | 17 April 2026 21:37:25 |
| Eccentricity: | 0.0101015 |
| inclination: | 47.2766° |
| perigee height: | 1523 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 168.3008° |
| argument of perigee: | 257.1061° |
| revolutions per day: | 12.17409357 |
| mean anomaly at epoch: | 101.8429° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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