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 07434U 26073.56366064 +.00000000 +00000-0 +11366-3 0 00005
2 07434 74.0439 107.3253 0021456 306.5609 53.3569 14.38191336 05
| Epoch (UTC): | 14 March 2026 13:31:40 |
| Eccentricity: | 0.0021456 |
| inclination: | 74.0439° |
| perigee height: | 749 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 107.3253° |
| argument of perigee: | 306.5609° |
| revolutions per day: | 14.38191336 |
| mean anomaly at epoch: | 53.3569° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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