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 43678U 26075.32640985 +.00000000 +00000-0 +17085-3 0 00002
2 43678 98.1036 267.6358 0012462 106.6473 253.6119 14.99996831 02
| Epoch (UTC): | 16 March 2026 07:50:01 |
| Eccentricity: | 0.0012462 |
| inclination: | 98.1036° |
| perigee height: | 558 km |
| apogee height: | 576 km |
| right ascension of ascending node: | 267.6358° |
| argument of perigee: | 106.6473° |
| revolutions per day: | 14.99996831 |
| mean anomaly at epoch: | 253.6119° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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