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 61901U 26145.60672132 +.00000000 +00000-0 +42666-3 0 00002
2 61901 97.4111 223.6262 0011486 117.0817 243.1597 15.31106505 08
| Epoch (UTC): | 25 May 2026 14:33:40 |
| Eccentricity: | 0.0011486 |
| inclination: | 97.4111° |
| perigee height: | 465 km |
| apogee height: | 480 km |
| right ascension of ascending node: | 223.6262° |
| argument of perigee: | 117.0817° |
| revolutions per day: | 15.31106505 |
| mean anomaly at epoch: | 243.1597° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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