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 54102U 26145.59411178 +.00000000 +00000-0 +49003-4 0 00009
2 54102 53.2137 348.8996 0001269 90.8199 269.2939 15.08834035 03
| Epoch (UTC): | 25 May 2026 14:15:31 |
| Eccentricity: | 0.0001269 |
| inclination: | 53.2137° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 348.8996° |
| argument of perigee: | 90.8199° |
| revolutions per day: | 15.08834035 |
| mean anomaly at epoch: | 269.2939° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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