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 61903U 26145.49821396 +.00000000 +00000-0 +49566-3 0 00005
2 61903 97.4110 222.5138 0011383 117.6080 242.6318 15.30035042 04
| Epoch (UTC): | 25 May 2026 11:57:25 |
| Eccentricity: | 0.0011383 |
| inclination: | 97.4110° |
| perigee height: | 468 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 222.5138° |
| argument of perigee: | 117.6080° |
| revolutions per day: | 15.30035042 |
| mean anomaly at epoch: | 242.6318° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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