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 40310U 26145.64626360 +.00000000 +00000-0 +72374-4 0 00009
2 40310 98.1455 282.7978 0013495 341.4805 18.5911 14.76188073 02
| Epoch (UTC): | 25 May 2026 15:30:37 |
| Eccentricity: | 0.0013495 |
| inclination: | 98.1455° |
| perigee height: | 632 km |
| apogee height: | 651 km |
| right ascension of ascending node: | 282.7978° |
| argument of perigee: | 341.4805° |
| revolutions per day: | 14.76188073 |
| mean anomaly at epoch: | 18.5911° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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