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 26156.49079029 +.00000000 +00000-0 +70526-3 0 00009
2 40054 98.2396 68.0471 0007409 260.5142 99.5247 15.08596254 09
| Epoch (UTC): | 05 June 2026 11:46:44 |
| Eccentricity: | 0.0007409 |
| inclination: | 98.2396° |
| perigee height: | 535 km |
| apogee height: | 546 km |
| right ascension of ascending node: | 68.0471° |
| argument of perigee: | 260.5142° |
| revolutions per day: | 15.08596254 |
| mean anomaly at epoch: | 99.5247° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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