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 53481U 26145.66668980 +.00000000 +00000-0 +37485-2 0 00000
2 53481 97.6045 267.6630 0001080 85.4730 358.9625 15.39750009 07
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001080 |
| inclination: | 97.6045° |
| perigee height: | 446 km |
| apogee height: | 448 km |
| right ascension of ascending node: | 267.6630° |
| argument of perigee: | 85.4730° |
| revolutions per day: | 15.39750009 |
| mean anomaly at epoch: | 358.9625° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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