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 60501U 26144.95944513 +.00000000 +00000-0 +38345-3 0 00008
2 60501 97.3698 228.8586 0003242 24.3661 335.7739 15.42102309 02
| Epoch (UTC): | 24 May 2026 23:01:36 |
| Eccentricity: | 0.0003242 |
| inclination: | 97.3698° |
| perigee height: | 438 km |
| apogee height: | 442 km |
| right ascension of ascending node: | 228.8586° |
| argument of perigee: | 24.3661° |
| revolutions per day: | 15.42102309 |
| mean anomaly at epoch: | 335.7739° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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