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 41105U 26156.06124634 +.00000000 +00000-0 +00000-0 0 00000
2 41105 6.6638 70.6705 0001332 281.5102 268.8844 1.00272317 08
| Epoch (UTC): | 05 June 2026 01:28:11 |
| Eccentricity: | 0.0001332 |
| inclination: | 6.6638° |
| perigee height: | 35781 km |
| apogee height: | 35792 km |
| right ascension of ascending node: | 70.6705° |
| argument of perigee: | 281.5102° |
| revolutions per day: | 1.00272317 |
| mean anomaly at epoch: | 268.8844° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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