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 01931U 26088.04915684 +.00000000 +00000-0 +26544-3 0 00002
2 01931 99.0149 121.0977 0235349 311.9603 46.1736 14.35024480 02
| Epoch (UTC): | 29 March 2026 01:10:47 |
| Eccentricity: | 0.0235349 |
| inclination: | 99.0149° |
| perigee height: | 607 km |
| apogee height: | 943 km |
| right ascension of ascending node: | 121.0977° |
| argument of perigee: | 311.9603° |
| revolutions per day: | 14.35024480 |
| mean anomaly at epoch: | 46.1736° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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