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 68632U 26145.32277213 +.00000000 +00000-0 +40724-3 0 00003
2 68632 60.0319 265.7556 0024584 11.7967 348.3684 15.25249881 07
| Epoch (UTC): | 25 May 2026 07:44:47 |
| Eccentricity: | 0.0024584 |
| inclination: | 60.0319° |
| perigee height: | 473 km |
| apogee height: | 507 km |
| right ascension of ascending node: | 265.7556° |
| argument of perigee: | 11.7967° |
| revolutions per day: | 15.25249881 |
| mean anomaly at epoch: | 348.3684° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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