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 31129U 26150.84746263 +.00000000 +00000-0 +32678-3 0 00002
2 31129 98.4527 130.1451 0083092 114.2538 246.7374 14.65859669 06
| Epoch (UTC): | 30 May 2026 20:20:20 |
| Eccentricity: | 0.0083092 |
| inclination: | 98.4527° |
| perigee height: | 616 km |
| apogee height: | 733 km |
| right ascension of ascending node: | 130.1451° |
| argument of perigee: | 114.2538° |
| revolutions per day: | 14.65859669 |
| mean anomaly at epoch: | 246.7374° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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