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 26073.46052449 +.00000000 +00000-0 +58588-3 0 00003
2 40025 98.1006 78.0660 0008912 177.3955 182.7325 15.16630587 01
| Epoch (UTC): | 14 March 2026 11:03:09 |
| Eccentricity: | 0.0008912 |
| inclination: | 98.1006° |
| perigee height: | 510 km |
| apogee height: | 522 km |
| right ascension of ascending node: | 78.0660° |
| argument of perigee: | 177.3955° |
| revolutions per day: | 15.16630587 |
| mean anomaly at epoch: | 182.7325° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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