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 49084U 26145.33096596 +.00000000 +00000-0 -77493-4 0 00002
2 49084 87.9154 10.4151 0001956 94.0021 266.1335 13.17652441 00
| Epoch (UTC): | 25 May 2026 07:56:35 |
| Eccentricity: | 0.0001956 |
| inclination: | 87.9154° |
| perigee height: | 1192 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.4151° |
| argument of perigee: | 94.0021° |
| revolutions per day: | 13.17652441 |
| mean anomaly at epoch: | 266.1335° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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