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 26053.83640692 +.00000000 +00000-0 +15912-3 0 00002
2 40037 97.9848 2.1725 0011325 325.8090 34.2400 14.95075000 01
| Epoch (UTC): | 22 February 2026 20:04:25 |
| Eccentricity: | 0.0011325 |
| inclination: | 97.9848° |
| perigee height: | 574 km |
| apogee height: | 590 km |
| right ascension of ascending node: | 2.1725° |
| argument of perigee: | 325.8090° |
| revolutions per day: | 14.95075000 |
| mean anomaly at epoch: | 34.2400° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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