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 49290U 26145.39991497 +.00000000 +00000-0 +27179-3 0 00005
2 49290 87.9172 278.9910 0001890 100.1934 259.9413 13.20770083 06
| Epoch (UTC): | 25 May 2026 09:35:52 |
| Eccentricity: | 0.0001890 |
| inclination: | 87.9172° |
| perigee height: | 1180 km |
| apogee height: | 1183 km |
| right ascension of ascending node: | 278.9910° |
| argument of perigee: | 100.1934° |
| revolutions per day: | 13.20770083 |
| mean anomaly at epoch: | 259.9413° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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