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 68831U 26143.06778800 +.00000000 +00000-0 +85958-3 0 00009
2 68831 55.0028 131.4537 0011288 4.5204 355.5916 15.19252245 07
| Epoch (UTC): | 23 May 2026 01:37:36 |
| Eccentricity: | 0.0011288 |
| inclination: | 55.0028° |
| perigee height: | 500 km |
| apogee height: | 516 km |
| right ascension of ascending node: | 131.4537° |
| argument of perigee: | 4.5204° |
| revolutions per day: | 15.19252245 |
| mean anomaly at epoch: | 355.5916° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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