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 54196U 26145.35673193 +.00000000 +00000-0 -44812-4 0 00007
2 54196 53.2120 9.8333 0001395 120.4118 239.7012 15.08843661 07
| Epoch (UTC): | 25 May 2026 08:33:41 |
| Eccentricity: | 0.0001395 |
| inclination: | 53.2120° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 9.8333° |
| argument of perigee: | 120.4118° |
| revolutions per day: | 15.08843661 |
| mean anomaly at epoch: | 239.7012° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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