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 40054U 26106.66183297 +.00000000 +00000-0 +35994-3 0 00006
2 40054 98.2434 14.6389 0011329 72.9731 287.2735 15.07622675 06
| Epoch (UTC): | 16 April 2026 15:53:02 |
| Eccentricity: | 0.0011329 |
| inclination: | 98.2434° |
| perigee height: | 536 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 14.6389° |
| argument of perigee: | 72.9731° |
| revolutions per day: | 15.07622675 |
| mean anomaly at epoch: | 287.2735° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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