View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 49738U 26145.45044164 +.00000000 +00000-0 +83216-3 0 00003
2 49738 53.2142 164.5233 0002414 47.5657 312.5539 15.10120137 08
| Epoch (UTC): | 25 May 2026 10:48:38 |
| Eccentricity: | 0.0002414 |
| inclination: | 53.2142° |
| perigee height: | 534 km |
| apogee height: | 538 km |
| right ascension of ascending node: | 164.5233° |
| argument of perigee: | 47.5657° |
| revolutions per day: | 15.10120137 |
| mean anomaly at epoch: | 312.5539° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|