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 25637U 26021.37825825 +.00000000 +00000-0 +29917-3 0 00008
2 25637 96.4864 311.4212 0137363 0.1982 109.4720 14.49131331 02
| Epoch (UTC): | 21 January 2026 09:04:41 |
| Eccentricity: | 0.0137363 |
| inclination: | 96.4864° |
| perigee height: | 631 km |
| apogee height: | 826 km |
| right ascension of ascending node: | 311.4212° |
| argument of perigee: | 0.1982° |
| revolutions per day: | 14.49131331 |
| mean anomaly at epoch: | 109.4720° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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