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 40024U 26066.03591817 +.00000000 +00000-0 +73577-3 0 00009
2 40024 98.0842 89.5850 0004368 155.6453 204.4991 15.27990956 00
| Epoch (UTC): | 07 March 2026 00:51:43 |
| Eccentricity: | 0.0004368 |
| inclination: | 98.0842° |
| perigee height: | 479 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 89.5850° |
| argument of perigee: | 155.6453° |
| revolutions per day: | 15.27990956 |
| mean anomaly at epoch: | 204.4991° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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