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 49100U 26145.60518385 +.00000000 +00000-0 -42482-4 0 00006
2 49100 87.9162 10.3409 0001911 96.1987 263.9362 13.17649277 06
| Epoch (UTC): | 25 May 2026 14:31:27 |
| Eccentricity: | 0.0001911 |
| inclination: | 87.9162° |
| perigee height: | 1192 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.3409° |
| argument of perigee: | 96.1987° |
| revolutions per day: | 13.17649277 |
| mean anomaly at epoch: | 263.9362° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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