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 68754U 26145.60546267 +.00000000 +00000-0 +14311-3 0 00000
2 68754 98.1197 293.2588 0012155 141.7987 218.4103 15.07266892 00
| Epoch (UTC): | 25 May 2026 14:31:51 |
| Eccentricity: | 0.0012155 |
| inclination: | 98.1197° |
| perigee height: | 536 km |
| apogee height: | 553 km |
| right ascension of ascending node: | 293.2588° |
| argument of perigee: | 141.7987° |
| revolutions per day: | 15.07266892 |
| mean anomaly at epoch: | 218.4103° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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