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 61603U 26145.64084970 +.00000000 +00000-0 +63381-3 0 00009
2 61603 87.8911 25.5531 0001044 88.8292 271.2955 13.11417905 02
| Epoch (UTC): | 25 May 2026 15:22:49 |
| Eccentricity: | 0.0001044 |
| inclination: | 87.8911° |
| perigee height: | 1217 km |
| apogee height: | 1218 km |
| right ascension of ascending node: | 25.5531° |
| argument of perigee: | 88.8292° |
| revolutions per day: | 13.11417905 |
| mean anomaly at epoch: | 271.2955° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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