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 26486U 26064.48694784 +.00000000 +00000-0 +00000-0 0 00007
2 26486 63.2172 248.7040 6712597 278.2750 13.5633 1.45766259 08
| Epoch (UTC): | 05 March 2026 11:41:12 |
| Eccentricity: | 0.6712597 |
| inclination: | 63.2172° |
| perigee height: | 4423 km |
| apogee height: | 48535 km |
| right ascension of ascending node: | 248.7040° |
| argument of perigee: | 278.2750° |
| revolutions per day: | 1.45766259 |
| mean anomaly at epoch: | 13.5633° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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