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 67868U 26145.54867707 +.00000000 +00000-0 +45730-3 0 00002
2 67868 53.1583 207.2024 0001025 71.1943 288.9169 15.30228595 05
| Epoch (UTC): | 25 May 2026 13:10:05 |
| Eccentricity: | 0.0001025 |
| inclination: | 53.1583° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 207.2024° |
| argument of perigee: | 71.1943° |
| revolutions per day: | 15.30228595 |
| mean anomaly at epoch: | 288.9169° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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