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 68898U 26145.26525296 +.00000000 +00000-0 +70733-3 0 00000
2 68898 97.2860 340.9603 0001511 86.8224 273.3200 15.49218946 02
| Epoch (UTC): | 25 May 2026 06:21:57 |
| Eccentricity: | 0.0001511 |
| inclination: | 97.2860° |
| perigee height: | 418 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 340.9603° |
| argument of perigee: | 86.8224° |
| revolutions per day: | 15.49218946 |
| mean anomaly at epoch: | 273.3200° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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