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 52687U 26145.29878444 +.00000000 +00000-0 +14740-4 0 00005
2 52687 53.2121 160.2100 0000656 82.5502 277.5564 15.08847136 02
| Epoch (UTC): | 25 May 2026 07:10:14 |
| Eccentricity: | 0.0000656 |
| inclination: | 53.2121° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 160.2100° |
| argument of perigee: | 82.5502° |
| revolutions per day: | 15.08847136 |
| mean anomaly at epoch: | 277.5564° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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