View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 13028U 26088.16354970 +.00000000 +00000-0 +11375-3 0 00006
2 13028 74.0394 237.1415 0020123 248.0298 111.8719 14.39889700 04
| Epoch (UTC): | 29 March 2026 03:55:30 |
| Eccentricity: | 0.0020123 |
| inclination: | 74.0394° |
| perigee height: | 745 km |
| apogee height: | 773 km |
| right ascension of ascending node: | 237.1415° |
| argument of perigee: | 248.0298° |
| revolutions per day: | 14.39889700 |
| mean anomaly at epoch: | 111.8719° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|