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 05435U 26088.18864931 +.00000000 +00000-0 +21784-3 0 00009
2 05435 50.1399 61.6956 0102052 245.0069 114.0234 14.60178457 03
| Epoch (UTC): | 29 March 2026 04:31:39 |
| Eccentricity: | 0.0102052 |
| inclination: | 50.1399° |
| perigee height: | 620 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 61.6956° |
| argument of perigee: | 245.0069° |
| revolutions per day: | 14.60178457 |
| mean anomaly at epoch: | 114.0234° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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