▸Orbital parameters

Orbit class	SSO
Inclination	97.2353°
Eccentricity	0.0016474
Period	93.2 min
Apogee	441 km
Perigee	418 km
Mean motion	15.45607390 rev/day
RAAN	39.9238°
Arg of perigee	152.0906°
Mean anomaly	208.1231°
B*	2.8714e-4
Rev at epoch	11,225

▸Two-line element set (TLE)

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

1 60207U 24125E 26188.05773411 .00013808 00000-0 28714-3 0 9997

2 60207 97.2353 39.9238 0016474 152.0906 208.1231 15.45607390112253

▸ source OMM (JSON)

{
  "OBJECT_NAME": "R5-S2",
  "OBJECT_ID": "2024-125E",
  "EPOCH": "2026-07-07T01:23:08.227+00:00",
  "MEAN_MOTION": 15.4560739,
  "ECCENTRICITY": 0.0016474,
  "INCLINATION": 97.2353,
  "RA_OF_ASC_NODE": 39.9238,
  "ARG_OF_PERICENTER": 152.0906,
  "MEAN_ANOMALY": 208.1231,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 60207,
  "REV_AT_EPOCH": 11225,
  "BSTAR": 0.00028714,
  "MEAN_MOTION_DOT": 0.00013808,
  "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	R5-S2
Operator	NASA Johnson Space Flight CenterHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Jul 4, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	7.26HIGHvia 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/60207

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