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 26070U 26158.73929330 +.00000000 +00000-0 -75326-4 0 00004
2 26070 71.0033 268.4903 0015054 37.9355 322.2825 14.15836821 03
| Epoch (UTC): | 07 June 2026 17:44:34 |
| Eccentricity: | 0.0015054 |
| inclination: | 71.0033° |
| perigee height: | 829 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 268.4903° |
| argument of perigee: | 37.9355° |
| revolutions per day: | 14.15836821 |
| mean anomaly at epoch: | 322.2825° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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