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 52462U 26145.50813163 +.00000000 +00000-0 +11336-3 0 00004
2 52462 53.2129 74.2771 0001214 86.9876 273.1255 15.08831085 07
| Epoch (UTC): | 25 May 2026 12:11:42 |
| Eccentricity: | 0.0001214 |
| inclination: | 53.2129° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 74.2771° |
| argument of perigee: | 86.9876° |
| revolutions per day: | 15.08831085 |
| mean anomaly at epoch: | 273.1255° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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