View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 61730U 26145.62966090 +.00000000 +00000-0 +13231-3 0 00009
2 61730 97.5588 69.4021 0003168 95.6475 264.5123 15.24708667 06
| Epoch (UTC): | 25 May 2026 15:06:42 |
| Eccentricity: | 0.0003168 |
| inclination: | 97.5588° |
| perigee height: | 489 km |
| apogee height: | 494 km |
| right ascension of ascending node: | 69.4021° |
| argument of perigee: | 95.6475° |
| revolutions per day: | 15.24708667 |
| mean anomaly at epoch: | 264.5123° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|