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 54052U 26145.50116201 +.00000000 +00000-0 +14835-4 0 00008
2 54052 53.2135 319.1122 0000955 106.5302 253.5795 15.08834882 05
| Epoch (UTC): | 25 May 2026 12:01:40 |
| Eccentricity: | 0.0000955 |
| inclination: | 53.2135° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 319.1122° |
| argument of perigee: | 106.5302° |
| revolutions per day: | 15.08834882 |
| mean anomaly at epoch: | 253.5795° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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