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 00115U 26100.20690257 +.00000000 +00000-0 +32849-3 0 00009
2 00115 48.1620 75.2217 0026971 311.5161 48.3443 14.97830396 03
| Epoch (UTC): | 10 April 2026 04:57:56 |
| Eccentricity: | 0.0026971 |
| inclination: | 48.1620° |
| perigee height: | 555 km |
| apogee height: | 592 km |
| right ascension of ascending node: | 75.2217° |
| argument of perigee: | 311.5161° |
| revolutions per day: | 14.97830396 |
| mean anomaly at epoch: | 48.3443° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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