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 26072.33308345 +.00000000 +00000-0 -73708-4 0 00004
2 26070 71.0005 90.1760 0016540 184.8331 175.2635 14.15825076 05
| Epoch (UTC): | 13 March 2026 07:59:38 |
| Eccentricity: | 0.0016540 |
| inclination: | 71.0005° |
| perigee height: | 828 km |
| apogee height: | 851 km |
| right ascension of ascending node: | 90.1760° |
| argument of perigee: | 184.8331° |
| revolutions per day: | 14.15825076 |
| mean anomaly at epoch: | 175.2635° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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