▸Orbital parameters

Orbit class	SSO
Inclination	97.3711°
Eccentricity	0.0004199
Period	93.3 min
Apogee	441 km
Perigee	435 km
Mean motion	15.42872074 rev/day
RAAN	271.8613°
Arg of perigee	184.7187°
Mean anomaly	175.4021°
B*	3.4086e-4
Rev at epoch	10,534

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 60497U 24149AF 26187.71472325 .00014884 00000-0 34086-3 0 9990

2 60497 97.3711 271.8613 0004199 184.7187 175.4021 15.42872074105346

▸ source OMM (JSON)

{
  "OBJECT_NAME": "FLOCK 4BE-32",
  "OBJECT_ID": "2024-149AF",
  "EPOCH": "2026-07-06T17:09:12.089+00:00",
  "MEAN_MOTION": 15.42872074,
  "ECCENTRICITY": 0.0004199,
  "INCLINATION": 97.3711,
  "RA_OF_ASC_NODE": 271.8613,
  "ARG_OF_PERICENTER": 184.7187,
  "MEAN_ANOMALY": 175.4021,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 60497,
  "REV_AT_EPOCH": 10534,
  "BSTAR": 0.00034086,
  "MEAN_MOTION_DOT": 0.00014884,
  "MEAN_MOTION_DDOT": 0
}

Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.

▸Satellite metadata

Name	FLOCK 4BE-32
Operator	Planet Labs, Inc. (Planet)HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Aug 16, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	5.7HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/60497

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.