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 26017.91519090 +.00000000 +00000-0 +35329-4 0 00007
2 07434 74.0436 209.7785 0019379 63.8676 296.4469 14.38153633 04
| Epoch (UTC): | 17 January 2026 21:57:52 |
| Eccentricity: | 0.0019379 |
| inclination: | 74.0436° |
| perigee height: | 751 km |
| apogee height: | 778 km |
| right ascension of ascending node: | 209.7785° |
| argument of perigee: | 63.8676° |
| revolutions per day: | 14.38153633 |
| mean anomaly at epoch: | 296.4469° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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