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 26113U 26062.14518066 +.00000000 +00000-0 +30215-2 0 00006
2 26113 94.1357 313.9399 7512345 299.9178 6.8844 1.68665517 08
| Epoch (UTC): | 03 March 2026 03:29:03 |
| Eccentricity: | 0.7512345 |
| inclination: | 94.1357° |
| perigee height: | 1038 km |
| apogee height: | 45829 km |
| right ascension of ascending node: | 313.9399° |
| argument of perigee: | 299.9178° |
| revolutions per day: | 1.68665517 |
| mean anomaly at epoch: | 6.8844° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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