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 40057U 26069.96219203 +.00000000 +00000-0 +50052-3 0 00009
2 40057 98.2621 329.4299 0006170 234.1944 125.8703 14.96882452 00
| Epoch (UTC): | 10 March 2026 23:05:33 |
| Eccentricity: | 0.0006170 |
| inclination: | 98.2621° |
| perigee height: | 572 km |
| apogee height: | 581 km |
| right ascension of ascending node: | 329.4299° |
| argument of perigee: | 234.1944° |
| revolutions per day: | 14.96882452 |
| mean anomaly at epoch: | 125.8703° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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