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 54172U 26145.03566632 +.00000000 +00000-0 -68150-4 0 00006
2 54172 53.2149 21.3617 0001595 88.5908 271.5267 15.08844840 05
| Epoch (UTC): | 25 May 2026 00:51:21 |
| Eccentricity: | 0.0001595 |
| inclination: | 53.2149° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 21.3617° |
| argument of perigee: | 88.5908° |
| revolutions per day: | 15.08844840 |
| mean anomaly at epoch: | 271.5267° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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