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 68918U 26145.11826993 +.00000000 +00000-0 +89941-3 0 00006
2 68918 97.2867 340.8543 0001023 106.8628 253.2735 15.49193539 03
| Epoch (UTC): | 25 May 2026 02:50:18 |
| Eccentricity: | 0.0001023 |
| inclination: | 97.2867° |
| perigee height: | 418 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 340.8543° |
| argument of perigee: | 106.8628° |
| revolutions per day: | 15.49193539 |
| mean anomaly at epoch: | 253.2735° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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