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 68251U 26144.92221248 +.00000000 +00000-0 +45348-3 0 00009
2 68251 53.1573 302.7893 0000919 83.7010 276.4095 15.30206134 06
| Epoch (UTC): | 24 May 2026 22:07:59 |
| Eccentricity: | 0.0000919 |
| inclination: | 53.1573° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 302.7893° |
| argument of perigee: | 83.7010° |
| revolutions per day: | 15.30206134 |
| mean anomaly at epoch: | 276.4095° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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