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 70014U 26065.42062500 +.00000000 +00000-0 -20078-2 0 00003
2 70014 53.1601 79.0033 0000549 71.7803 323.6555 16.02937959 06
| Epoch (UTC): | 06 March 2026 10:05:42 |
| Eccentricity: | 0.0000549 |
| inclination: | 53.1601° |
| perigee height: | 266 km |
| apogee height: | 267 km |
| right ascension of ascending node: | 79.0033° |
| argument of perigee: | 71.7803° |
| revolutions per day: | 16.02937959 |
| mean anomaly at epoch: | 323.6555° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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