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 26064.21060365 +.00000000 +00000-0 +13743-3 0 00008
2 25682 97.8607 72.6096 0001743 85.0336 338.7845 14.63814551 08
| Epoch (UTC): | 05 March 2026 05:03:16 |
| Eccentricity: | 0.0001743 |
| inclination: | 97.8607° |
| perigee height: | 680 km |
| apogee height: | 682 km |
| right ascension of ascending node: | 72.6096° |
| argument of perigee: | 85.0336° |
| revolutions per day: | 14.63814551 |
| mean anomaly at epoch: | 338.7845° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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