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 25635U 26146.26343392 +.00000000 +00000-0 +96827-4 0 00001
2 25635 96.4836 58.7568 0130193 256.8032 101.8617 14.51787494 05
| Epoch (UTC): | 26 May 2026 06:19:20 |
| Eccentricity: | 0.0130193 |
| inclination: | 96.4836° |
| perigee height: | 627 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 58.7568° |
| argument of perigee: | 256.8032° |
| revolutions per day: | 14.51787494 |
| mean anomaly at epoch: | 101.8617° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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