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 41948U 26156.63246799 +.00000000 +00000-0 -99469-4 0 00007
2 41948 97.4122 216.1531 0003728 285.1069 74.9753 15.19236200 07
| Epoch (UTC): | 05 June 2026 15:10:45 |
| Eccentricity: | 0.0003728 |
| inclination: | 97.4122° |
| perigee height: | 506 km |
| apogee height: | 511 km |
| right ascension of ascending node: | 216.1531° |
| argument of perigee: | 285.1069° |
| revolutions per day: | 15.19236200 |
| mean anomaly at epoch: | 74.9753° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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