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 40070U 26156.47760557 +.00000000 +00000-0 +15594-3 0 00002
2 40070 98.0690 134.7781 0131589 105.0247 256.5557 14.55637289 07
| Epoch (UTC): | 05 June 2026 11:27:45 |
| Eccentricity: | 0.0131589 |
| inclination: | 98.0690° |
| perigee height: | 614 km |
| apogee height: | 801 km |
| right ascension of ascending node: | 134.7781° |
| argument of perigee: | 105.0247° |
| revolutions per day: | 14.55637289 |
| mean anomaly at epoch: | 256.5557° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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