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 40025U 26018.94044308 +.00000000 +00000-0 +53087-3 0 00009
2 40025 98.0974 19.9221 0010135 26.9742 333.2014 15.15254453 05
| Epoch (UTC): | 18 January 2026 22:34:14 |
| Eccentricity: | 0.0010135 |
| inclination: | 98.0974° |
| perigee height: | 513 km |
| apogee height: | 527 km |
| right ascension of ascending node: | 19.9221° |
| argument of perigee: | 26.9742° |
| revolutions per day: | 15.15254453 |
| mean anomaly at epoch: | 333.2014° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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