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 54199U 26145.02921494 +.00000000 +00000-0 -23486-4 0 00008
2 54199 53.2149 11.3405 0001194 114.5473 245.5644 15.08842609 01
| Epoch (UTC): | 25 May 2026 00:42:04 |
| Eccentricity: | 0.0001194 |
| inclination: | 53.2149° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 11.3405° |
| argument of perigee: | 114.5473° |
| revolutions per day: | 15.08842609 |
| mean anomaly at epoch: | 245.5644° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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