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 31797U 26146.24485769 +.00000000 +00000-0 +67115-3 0 00007
2 31797 98.1016 248.0262 0012585 181.3055 178.8162 15.46688388 02
| Epoch (UTC): | 26 May 2026 05:52:35 |
| Eccentricity: | 0.0012585 |
| inclination: | 98.1016° |
| perigee height: | 418 km |
| apogee height: | 435 km |
| right ascension of ascending node: | 248.0262° |
| argument of perigee: | 181.3055° |
| revolutions per day: | 15.46688388 |
| mean anomaly at epoch: | 178.8162° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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