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 28054U 26140.59716354 +.00000000 +00000-0 +18825-5 0 00004
2 28054 98.9906 164.2411 0006299 217.8340 304.2323 14.14479740 00
| Epoch (UTC): | 20 May 2026 14:19:54 |
| Eccentricity: | 0.0006299 |
| inclination: | 98.9906° |
| perigee height: | 840 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 164.2411° |
| argument of perigee: | 217.8340° |
| revolutions per day: | 14.14479740 |
| mean anomaly at epoch: | 304.2323° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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