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 52939U 26145.44173755 +.00000000 +00000-0 +25231-3 0 00001
2 52939 9.9517 243.5847 0024129 221.4109 138.4276 15.23773216 09
| Epoch (UTC): | 25 May 2026 10:36:06 |
| Eccentricity: | 0.0024129 |
| inclination: | 9.9517° |
| perigee height: | 478 km |
| apogee height: | 511 km |
| right ascension of ascending node: | 243.5847° |
| argument of perigee: | 221.4109° |
| revolutions per day: | 15.23773216 |
| mean anomaly at epoch: | 138.4276° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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