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 62512U 26145.56061135 +.00000000 +00000-0 +19255-2 0 00008
2 62512 42.9998 327.7982 0005313 286.5613 73.4671 15.70832046 04
| Epoch (UTC): | 25 May 2026 13:27:16 |
| Eccentricity: | 0.0005313 |
| inclination: | 42.9998° |
| perigee height: | 353 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 327.7982° |
| argument of perigee: | 286.5613° |
| revolutions per day: | 15.70832046 |
| mean anomaly at epoch: | 73.4671° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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