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 00029U 26158.47064684 +.00000000 +00000-0 +10527-3 0 00003
2 00029 48.3787 70.8231 0022455 227.9748 131.9254 14.78763763 05
| Epoch (UTC): | 07 June 2026 11:17:43 |
| Eccentricity: | 0.0022455 |
| inclination: | 48.3787° |
| perigee height: | 617 km |
| apogee height: | 649 km |
| right ascension of ascending node: | 70.8231° |
| argument of perigee: | 227.9748° |
| revolutions per day: | 14.78763763 |
| mean anomaly at epoch: | 131.9254° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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