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 68200U 26137.95813361 +.00000000 +00000-0 +16257-3 0 00008
2 68200 97.5323 213.2139 0009986 65.3258 294.9010 15.10452253 02
| Epoch (UTC): | 17 May 2026 22:59:42 |
| Eccentricity: | 0.0009986 |
| inclination: | 97.5323° |
| perigee height: | 528 km |
| apogee height: | 542 km |
| right ascension of ascending node: | 213.2139° |
| argument of perigee: | 65.3258° |
| revolutions per day: | 15.10452253 |
| mean anomaly at epoch: | 294.9010° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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