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 31128U 26038.86862465 +.00000000 +00000-0 +32869-3 0 00003
2 31128 98.4234 5.8584 0086463 123.0462 237.9082 14.63391620 08
| Epoch (UTC): | 07 February 2026 20:50:49 |
| Eccentricity: | 0.0086463 |
| inclination: | 98.4234° |
| perigee height: | 621 km |
| apogee height: | 743 km |
| right ascension of ascending node: | 5.8584° |
| argument of perigee: | 123.0462° |
| revolutions per day: | 14.63391620 |
| mean anomaly at epoch: | 237.9082° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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