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 52486U 26145.52189720 +.00000000 +00000-0 +52968-3 0 00003
2 52486 53.2137 74.2047 0001407 96.0587 264.0565 15.08806508 08
| Epoch (UTC): | 25 May 2026 12:31:31 |
| Eccentricity: | 0.0001407 |
| inclination: | 53.2137° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 74.2047° |
| argument of perigee: | 96.0587° |
| revolutions per day: | 15.08806508 |
| mean anomaly at epoch: | 264.0565° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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