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 00202U 26149.21206465 +.00000000 +00000-0 +44928-4 0 00006
2 00202 32.4365 97.3381 0100747 70.7736 290.3755 13.63791310 04
| Epoch (UTC): | 29 May 2026 05:05:22 |
| Eccentricity: | 0.0100747 |
| inclination: | 32.4365° |
| perigee height: | 947 km |
| apogee height: | 1097 km |
| right ascension of ascending node: | 97.3381° |
| argument of perigee: | 70.7736° |
| revolutions per day: | 13.63791310 |
| mean anomaly at epoch: | 290.3755° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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