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 52202U 26145.64258184 +.00000000 +00000-0 +18045-4 0 00002
2 52202 67.1485 283.4910 0005774 258.4671 101.5765 13.96678283 05
| Epoch (UTC): | 25 May 2026 15:25:19 |
| Eccentricity: | 0.0005774 |
| inclination: | 67.1485° |
| perigee height: | 901 km |
| apogee height: | 910 km |
| right ascension of ascending node: | 283.4910° |
| argument of perigee: | 258.4671° |
| revolutions per day: | 13.96678283 |
| mean anomaly at epoch: | 101.5765° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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