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 49200U 26145.64319758 +.00000000 +00000-0 +22354-3 0 00008
2 49200 87.9170 278.9419 0001179 76.2774 283.8490 13.20769288 00
| Epoch (UTC): | 25 May 2026 15:26:12 |
| Eccentricity: | 0.0001179 |
| inclination: | 87.9170° |
| perigee height: | 1181 km |
| apogee height: | 1183 km |
| right ascension of ascending node: | 278.9419° |
| argument of perigee: | 76.2774° |
| revolutions per day: | 13.20769288 |
| mean anomaly at epoch: | 283.8490° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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