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 40015U 26145.48305433 +.00000000 +00000-0 +11053-3 0 00004
2 40015 97.6401 309.4414 0034290 70.4809 290.0105 14.85334209 06
| Epoch (UTC): | 25 May 2026 11:35:35 |
| Eccentricity: | 0.0034290 |
| inclination: | 97.6401° |
| perigee height: | 589 km |
| apogee height: | 637 km |
| right ascension of ascending node: | 309.4414° |
| argument of perigee: | 70.4809° |
| revolutions per day: | 14.85334209 |
| mean anomaly at epoch: | 290.0105° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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