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 40074U 26075.23576448 +.00000000 +00000-0 +54240-3 0 00005
2 40074 98.4236 68.8644 0003383 101.5078 258.6529 15.11947317 00
| Epoch (UTC): | 16 March 2026 05:39:30 |
| Eccentricity: | 0.0003383 |
| inclination: | 98.4236° |
| perigee height: | 528 km |
| apogee height: | 533 km |
| right ascension of ascending node: | 68.8644° |
| argument of perigee: | 101.5078° |
| revolutions per day: | 15.11947317 |
| mean anomaly at epoch: | 258.6529° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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