View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 56130U 26145.21132553 +.00000000 +00000-0 +33425-4 0 00009
2 56130 43.0047 74.7917 0001268 268.5992 91.4714 15.27576965 07
| Epoch (UTC): | 25 May 2026 05:04:18 |
| Eccentricity: | 0.0001268 |
| inclination: | 43.0047° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 74.7917° |
| argument of perigee: | 268.5992° |
| revolutions per day: | 15.27576965 |
| mean anomaly at epoch: | 91.4714° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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