View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 49428U 26145.55775691 +.00000000 +00000-0 -12011-4 0 00003
2 49428 53.2141 243.9583 0001221 84.8067 275.3064 15.08838380 09
| Epoch (UTC): | 25 May 2026 13:23:10 |
| Eccentricity: | 0.0001221 |
| inclination: | 53.2141° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 243.9583° |
| argument of perigee: | 84.8067° |
| revolutions per day: | 15.08838380 |
| mean anomaly at epoch: | 275.3064° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|