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 52539U 26145.47147252 +.00000000 +00000-0 -19392-2 0 00004
2 52539 53.2135 144.4336 0001998 51.2152 308.9018 15.08624876 09
| Epoch (UTC): | 25 May 2026 11:18:55 |
| Eccentricity: | 0.0001998 |
| inclination: | 53.2135° |
| perigee height: | 539 km |
| apogee height: | 542 km |
| right ascension of ascending node: | 144.4336° |
| argument of perigee: | 51.2152° |
| revolutions per day: | 15.08624876 |
| mean anomaly at epoch: | 308.9018° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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