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 26053.67571534 +.00000000 +00000-0 +99224-3 0 00009
2 40054 98.2462 317.9226 0008039 246.7503 113.2876 15.06274907 02
| Epoch (UTC): | 22 February 2026 16:13:01 |
| Eccentricity: | 0.0008039 |
| inclination: | 98.2462° |
| perigee height: | 542 km |
| apogee height: | 553 km |
| right ascension of ascending node: | 317.9226° |
| argument of perigee: | 246.7503° |
| revolutions per day: | 15.06274907 |
| mean anomaly at epoch: | 113.2876° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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