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 68980U 26145.62160036 +.00000000 +00000-0 +16494-3 0 00003
2 68980 97.7389 43.4548 0006212 211.9557 148.1285 14.90462939 01
| Epoch (UTC): | 25 May 2026 14:55:06 |
| Eccentricity: | 0.0006212 |
| inclination: | 97.7389° |
| perigee height: | 592 km |
| apogee height: | 601 km |
| right ascension of ascending node: | 43.4548° |
| argument of perigee: | 211.9557° |
| revolutions per day: | 14.90462939 |
| mean anomaly at epoch: | 148.1285° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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