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 68489U 26145.32413826 +.00000000 +00000-0 +27091-3 0 00007
2 68489 97.7522 103.8601 0003458 116.8720 243.2853 14.91470288 04
| Epoch (UTC): | 25 May 2026 07:46:45 |
| Eccentricity: | 0.0003458 |
| inclination: | 97.7522° |
| perigee height: | 591 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 103.8601° |
| argument of perigee: | 116.8720° |
| revolutions per day: | 14.91470288 |
| mean anomaly at epoch: | 243.2853° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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