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 26088.20079994 +.00000000 +00000-0 +20006-3 0 00006
2 43678 98.1040 281.0392 0013602 68.9726 291.2950 15.00056761 06
| Epoch (UTC): | 29 March 2026 04:49:09 |
| Eccentricity: | 0.0013602 |
| inclination: | 98.1040° |
| perigee height: | 557 km |
| apogee height: | 576 km |
| right ascension of ascending node: | 281.0392° |
| argument of perigee: | 68.9726° |
| revolutions per day: | 15.00056761 |
| mean anomaly at epoch: | 291.2950° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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