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 54162U 26145.37331660 +.00000000 +00000-0 +53070-4 0 00007
2 54162 53.2124 29.8876 0001218 85.2376 274.8755 15.08826028 08
| Epoch (UTC): | 25 May 2026 08:57:34 |
| Eccentricity: | 0.0001218 |
| inclination: | 53.2124° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 29.8876° |
| argument of perigee: | 85.2376° |
| revolutions per day: | 15.08826028 |
| mean anomaly at epoch: | 274.8755° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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