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 40072U 26087.83018725 +.00000000 +00000-0 +20380-3 0 00009
2 40072 98.3759 42.2670 0005685 165.3620 194.7760 14.87796013 04
| Epoch (UTC): | 28 March 2026 19:55:28 |
| Eccentricity: | 0.0005685 |
| inclination: | 98.3759° |
| perigee height: | 601 km |
| apogee height: | 609 km |
| right ascension of ascending node: | 42.2670° |
| argument of perigee: | 165.3620° |
| revolutions per day: | 14.87796013 |
| mean anomaly at epoch: | 194.7760° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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