View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 52988U 26145.14883618 +.00000000 +00000-0 +58717-4 0 00004
2 52988 53.2140 110.8792 0000501 52.9449 307.1589 15.08848417 05
| Epoch (UTC): | 25 May 2026 03:34:19 |
| Eccentricity: | 0.0000501 |
| inclination: | 53.2140° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 110.8792° |
| argument of perigee: | 52.9449° |
| revolutions per day: | 15.08848417 |
| mean anomaly at epoch: | 307.1589° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|