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 61248U 26145.11605918 +.00000000 +00000-0 +28268-4 0 00003
2 61248 53.1595 39.2491 0000989 78.3490 281.7639 15.69706203 01
| Epoch (UTC): | 25 May 2026 02:47:07 |
| Eccentricity: | 0.0000989 |
| inclination: | 53.1595° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 39.2491° |
| argument of perigee: | 78.3490° |
| revolutions per day: | 15.69706203 |
| mean anomaly at epoch: | 281.7639° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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