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 25479U 26121.48772277 +.00000000 +00000-0 +33733-3 0 00008
2 25479 45.0061 197.0741 0002276 25.2183 334.8776 14.39005791 09
| Epoch (UTC): | 01 May 2026 11:42:19 |
| Eccentricity: | 0.0002276 |
| inclination: | 45.0061° |
| perigee height: | 760 km |
| apogee height: | 763 km |
| right ascension of ascending node: | 197.0741° |
| argument of perigee: | 25.2183° |
| revolutions per day: | 14.39005791 |
| mean anomaly at epoch: | 334.8776° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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