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 40037U 26106.90520501 +.00000000 +00000-0 -12058-5 0 00006
2 40037 97.9917 56.2269 0012540 136.7259 223.4949 14.95314827 00
| Epoch (UTC): | 16 April 2026 21:43:29 |
| Eccentricity: | 0.0012540 |
| inclination: | 97.9917° |
| perigee height: | 573 km |
| apogee height: | 590 km |
| right ascension of ascending node: | 56.2269° |
| argument of perigee: | 136.7259° |
| revolutions per day: | 14.95314827 |
| mean anomaly at epoch: | 223.4949° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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