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 40014U 26072.60249911 +.00000000 +00000-0 +31645-3 0 00003
2 40014 98.0423 159.6490 0029476 145.3481 214.9677 15.14554752 00
| Epoch (UTC): | 13 March 2026 14:27:35 |
| Eccentricity: | 0.0029476 |
| inclination: | 98.0423° |
| perigee height: | 502 km |
| apogee height: | 543 km |
| right ascension of ascending node: | 159.6490° |
| argument of perigee: | 145.3481° |
| revolutions per day: | 15.14554752 |
| mean anomaly at epoch: | 214.9677° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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