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 40958U 26150.58863176 +.00000000 +00000-0 +78212-4 0 00001
2 40958 97.6671 144.8355 0016477 334.9213 25.1196 14.76757490 08
| Epoch (UTC): | 30 May 2026 14:07:37 |
| Eccentricity: | 0.0016477 |
| inclination: | 97.6671° |
| perigee height: | 628 km |
| apogee height: | 651 km |
| right ascension of ascending node: | 144.8355° |
| argument of perigee: | 334.9213° |
| revolutions per day: | 14.76757490 |
| mean anomaly at epoch: | 25.1196° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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