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 02142U 26104.01352104 +.00000000 +00000-0 +34058-4 0 00005
2 02142 35.0467 321.0679 0006625 159.1209 200.9750 14.34683115 09
| Epoch (UTC): | 14 April 2026 00:19:28 |
| Eccentricity: | 0.0006625 |
| inclination: | 35.0467° |
| perigee height: | 771 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 321.0679° |
| argument of perigee: | 159.1209° |
| revolutions per day: | 14.34683115 |
| mean anomaly at epoch: | 200.9750° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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