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 52123U 26145.24957905 +.00000000 +00000-0 +67452-4 0 00003
2 52123 53.2126 85.2517 0001189 113.2912 246.8206 15.08842402 02
| Epoch (UTC): | 25 May 2026 05:59:23 |
| Eccentricity: | 0.0001189 |
| inclination: | 53.2126° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 85.2517° |
| argument of perigee: | 113.2912° |
| revolutions per day: | 15.08842402 |
| mean anomaly at epoch: | 246.8206° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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