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 61213U 26145.21486808 +.00000000 +00000-0 +16095-2 0 00004
2 61213 53.1613 326.3703 0001104 61.9385 298.1729 15.34154994 09
| Epoch (UTC): | 25 May 2026 05:09:24 |
| Eccentricity: | 0.0001104 |
| inclination: | 53.1613° |
| perigee height: | 463 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 326.3703° |
| argument of perigee: | 61.9385° |
| revolutions per day: | 15.34154994 |
| mean anomaly at epoch: | 298.1729° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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