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 52554U 26145.41378953 +.00000000 +00000-0 +32413-4 0 00009
2 52554 53.2136 149.6905 0000636 103.8407 256.2655 15.08845409 00
| Epoch (UTC): | 25 May 2026 09:55:51 |
| Eccentricity: | 0.0000636 |
| inclination: | 53.2136° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 149.6905° |
| argument of perigee: | 103.8407° |
| revolutions per day: | 15.08845409 |
| mean anomaly at epoch: | 256.2655° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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