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 25693U 26039.13794654 +.00000000 +00000-0 +96960-4 0 00001
2 25693 64.5543 100.2575 0038068 237.4198 122.3231 14.84108167 07
| Epoch (UTC): | 08 February 2026 03:18:38 |
| Eccentricity: | 0.0038068 |
| inclination: | 64.5543° |
| perigee height: | 590 km |
| apogee height: | 643 km |
| right ascension of ascending node: | 100.2575° |
| argument of perigee: | 237.4198° |
| revolutions per day: | 14.84108167 |
| mean anomaly at epoch: | 122.3231° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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