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 61048U 26145.05091169 +.00000000 +00000-0 +31115-3 0 00005
2 61048 52.9788 55.5318 0008921 55.8776 304.3063 15.20727766 07
| Epoch (UTC): | 25 May 2026 01:13:18 |
| Eccentricity: | 0.0008921 |
| inclination: | 52.9788° |
| perigee height: | 498 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 55.5318° |
| argument of perigee: | 55.8776° |
| revolutions per day: | 15.20727766 |
| mean anomaly at epoch: | 304.3063° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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