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 68763U 26145.60166419 +.00000000 +00000-0 +19309-3 0 00009
2 68763 97.7764 283.3875 0010888 126.8063 233.4165 15.07370061 03
| Epoch (UTC): | 25 May 2026 14:26:23 |
| Eccentricity: | 0.0010888 |
| inclination: | 97.7764° |
| perigee height: | 537 km |
| apogee height: | 552 km |
| right ascension of ascending node: | 283.3875° |
| argument of perigee: | 126.8063° |
| revolutions per day: | 15.07370061 |
| mean anomaly at epoch: | 233.4165° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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