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 40032U 26101.24692265 +.00000000 +00000-0 +35508-3 0 00002
2 40032 98.0756 94.0127 0008913 53.2470 306.9577 15.14298563 02
| Epoch (UTC): | 11 April 2026 05:55:34 |
| Eccentricity: | 0.0008913 |
| inclination: | 98.0756° |
| perigee height: | 517 km |
| apogee height: | 529 km |
| right ascension of ascending node: | 94.0127° |
| argument of perigee: | 53.2470° |
| revolutions per day: | 15.14298563 |
| mean anomaly at epoch: | 306.9577° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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