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 26075.24187993 +.00000000 +00000-0 +45371-3 0 00000
2 40025 98.1001 79.9679 0009107 172.1539 187.9837 15.16666180 07
| Epoch (UTC): | 16 March 2026 05:48:18 |
| Eccentricity: | 0.0009107 |
| inclination: | 98.1001° |
| perigee height: | 510 km |
| apogee height: | 522 km |
| right ascension of ascending node: | 79.9679° |
| argument of perigee: | 172.1539° |
| revolutions per day: | 15.16666180 |
| mean anomaly at epoch: | 187.9837° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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