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 26088.21757991 +.00000000 +00000-0 +22973-3 0 00005
2 40070 98.0643 68.7861 0129503 317.8917 41.2385 14.55566306 09
| Epoch (UTC): | 29 March 2026 05:13:18 |
| Eccentricity: | 0.0129503 |
| inclination: | 98.0643° |
| perigee height: | 616 km |
| apogee height: | 799 km |
| right ascension of ascending node: | 68.7861° |
| argument of perigee: | 317.8917° |
| revolutions per day: | 14.55566306 |
| mean anomaly at epoch: | 41.2385° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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