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 68903U 26145.43154177 +.00000000 +00000-0 +76077-3 0 00009
2 68903 97.2864 341.1934 0002179 92.0152 268.1348 15.49220471 04
| Epoch (UTC): | 25 May 2026 10:21:25 |
| Eccentricity: | 0.0002179 |
| inclination: | 97.2864° |
| perigee height: | 418 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 341.1934° |
| argument of perigee: | 92.0152° |
| revolutions per day: | 15.49220471 |
| mean anomaly at epoch: | 268.1348° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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