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 26088.18255644 +.00000000 +00000-0 +12072-3 0 00003
2 40958 97.6676 85.5347 0017151 167.0928 193.0725 14.76671347 02
| Epoch (UTC): | 29 March 2026 04:22:52 |
| Eccentricity: | 0.0017151 |
| inclination: | 97.6676° |
| perigee height: | 628 km |
| apogee height: | 652 km |
| right ascension of ascending node: | 85.5347° |
| argument of perigee: | 167.0928° |
| revolutions per day: | 14.76671347 |
| mean anomaly at epoch: | 193.0725° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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