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 25682U 26067.15002943 +.00000000 +00000-0 +15676-3 0 00009
2 25682 97.8609 75.4143 0001719 83.2194 341.3072 14.63819564 00
| Epoch (UTC): | 08 March 2026 03:36:02 |
| Eccentricity: | 0.0001719 |
| inclination: | 97.8609° |
| perigee height: | 680 km |
| apogee height: | 682 km |
| right ascension of ascending node: | 75.4143° |
| argument of perigee: | 83.2194° |
| revolutions per day: | 14.63819564 |
| mean anomaly at epoch: | 341.3072° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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