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 26108.28819353 +.00000000 +00000-0 +31663-3 0 00002
2 40025 98.0993 115.2745 0010634 75.2031 285.0379 15.17299257 00
| Epoch (UTC): | 18 April 2026 06:54:59 |
| Eccentricity: | 0.0010634 |
| inclination: | 98.0993° |
| perigee height: | 507 km |
| apogee height: | 521 km |
| right ascension of ascending node: | 115.2745° |
| argument of perigee: | 75.2031° |
| revolutions per day: | 15.17299257 |
| mean anomaly at epoch: | 285.0379° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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