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 12435U 26088.08445803 +.00000000 +00000-0 +17619-4 0 00002
2 12435 64.7704 330.4361 0035090 254.7726 104.9456 13.93190258 05
| Epoch (UTC): | 29 March 2026 02:01:37 |
| Eccentricity: | 0.0035090 |
| inclination: | 64.7704° |
| perigee height: | 892 km |
| apogee height: | 943 km |
| right ascension of ascending node: | 330.4361° |
| argument of perigee: | 254.7726° |
| revolutions per day: | 13.93190258 |
| mean anomaly at epoch: | 104.9456° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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