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 49219U 26145.32755286 +.00000000 +00000-0 +19930-3 0 00009
2 49219 87.9176 278.9900 0001690 100.8206 259.3117 13.20772077 07
| Epoch (UTC): | 25 May 2026 07:51:40 |
| Eccentricity: | 0.0001690 |
| inclination: | 87.9176° |
| perigee height: | 1180 km |
| apogee height: | 1183 km |
| right ascension of ascending node: | 278.9900° |
| argument of perigee: | 100.8206° |
| revolutions per day: | 13.20772077 |
| mean anomaly at epoch: | 259.3117° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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